Cargo Mate

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CARGO Mate File Definitions ASTM - Volume Converter (1) ASTM - Volume Converter (2) API Converter Blended API COMINGLE-LOADING (1) COMINGLE-LOADING (2) Shore Line Displasement Draft Converter Change of Draft due to List Filling Rate Volume of Pipe & Max.Rate Volume of Cargo Lines (1) Volume of Cargo Lines (2) Volume Calc Temperature Converter Conversion Factors (Brown's) Units Converter ET Completion of Cargo Op. Conversion Tables Crude Oil Volume of Pipelines (SGS)

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Various Tables

Transcript of Cargo Mate

Page 1: Cargo Mate

CARGO Mate File (Version 27/05/2007)

Definitions Definitions

ASTM - Volume Converter (1) ASTM - Volume Converter (1)

ASTM - Volume Converter (2) ASTM - Volume Converter (2)

API Converter API Converter

Blended API Blended API

COMINGLE-LOADING (1) COMINGLE-LOADING (1)

COMINGLE-LOADING (2) COMINGLE-LOADING (2)

Shore Line Displasement Shore Line Displasement

Draft Converter Draft Converter

Change of Draft due to List Change of Draft due to List

Filling Rate Filling Rate

Volume of Pipe & Max.Rate Volume of Pipe & Max.Rate

Volume of Cargo Lines (1) Volume of Cargo Lines (1)

Volume of Cargo Lines (2) Volume of Cargo Lines (2)

Volume Calc Volume Calc

Temperature Converter Temperature Converter

Conversion Factors (Brown's) Conversion Factors (Brown's)

Units Converter Units Converter

ET Completion of Cargo Op. ET Completion of Cargo Op.

Conversion Tables Crude Oil Conversion Tables Crude Oil

Volume of Pipelines (SGS) Volume of Pipelines (SGS)

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CARGO Mate File (Version 27/05/2007)

ASTM Table 1 ASTM Table 1

ASTM T. 3, 4, 8, 11, 12, 13 ASTM T. 3, 4, 8, 11, 12, 13

ASTM T. 21, 29, 51, 52, 56 ASTM T. 21, 29, 51, 52, 56

ASTM T. 6 ASTM T. 6

ASTM T. 6A ASTM T. 6A

ASTM T. 6B ASTM T. 6B

ASTM T. 54A ASTM T. 54A

ASTM T. 54B ASTM T. 54B

ASTM T. 4, 11, 13, 52, 57 ASTM T. 4, 11, 13, 52, 57

Wedge Formulas Wedge Formulas

Wedge Formula Saybolt Wedge Formula Saybolt

Wedge Formula 1 Wedge Formula 1

Wedge Calc 1 Wedge Calc 1

Wedge Calc 2 Wedge Calc 2

Wedge Calc 3 Wedge Calc 3

Note

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DEFINITIONS

A.P.I. Gravity @60°F:The A.P.I. Gravity of an oil is derived from an equation which relies upon the Specific Gravity or Relative Density of the oil. As the equation relies upon a parameter which has no units (as it is a ratio) this parameter also has no units and is only a factor without any scientific meaning. It is believed that it was originally derived for oil trading purposes for price fixing i.e. the higher the A.P.I, the higher the price for the oil.

DENSITYDensity is by definition measured in vacuum at 15°C.Use tablles 54A or 54B in volumes VII and VIII.

Density - this parameter is normally recorded at the standard measurement/calculation temperature of 15°C. Its units are reported as either kilograms per litre (kg/ltr) or more correctly kilograms per cubic meter (kg/m3). This parameter gives the ratio of the mass of the oil to its volume albeit that its units record an apparent weight per unit volume. The Density of an oil is normally reported on a certificate of quality to four decimal places as say, 0.8590 kg/ltr. @ 15°C. It is the preferred parameter for the calculation of quantity of the oil cargo.

Reference to density "in vacuo" and density "in air" is to be specifically avoided.The standard parameter of density is only density (to be associated with density "in vacuo") and density "in air" does not exist save for its associated Petroleum Measurement table 56 factor for tonnage calculation/conversion.

RELATIVE DENSITY 15/4Relative Density 15/4 is the density of oil at 15°C/density of fresh water at 4°C.Relative Density 15/4 can be treated exactly the same way as density at 15°C as it is almost the same.Use tablles 54A or 54B in volumes VII and VIII or convert to API using table 3 in volume XI/XII.

RELATIVE DENSITY 60/60 (SG)Relative Density 60/60 is the density of cargo at 60°F/density of fresh water at 60°F.Convert this density at 15°C, or API using table 3 in volume XI/XII.

Specific Gravity - this parameter is more correctly identified and termed Relative Density. The parameter has no units as it is the ratio of the Density of oil at a temperature to the Density of water at a temperature (thus the correct terminology of Relative Density). Commonly the recorded temperatures are 60/60°F but alternative temperatures of 15/4°C may also be found. This latter Relative Density is in fact Density @ 15°C given that the Density of water at 4°C is 1.00.

ASTM Tables- Table 5A, 6A, 23A, 24A, 53A, and 54A are ASTM tables for Crude Oils- Table 5B, 6B, 23B, 24B, 53B, and 54B are ASTM tables for Petroleum products.- Table 5C, 24C and 54C are ASTM tables USING Thermal Expansion Coefficients.- Table 5D, 6D, 53D and 54D are ASTM tables for Lubrication Oils.- The ODD tables are for converting API, Relative Density or Density into API60, RD60 or DENS15.

If using Table 11 together with API60/60 and Stowfactor Longtons per Barrel, the result will be weight in longtons and in AIR.

If using Table 13 together with API60/60 and Stowfactor Tonnes per Barrel, the result will be weight in Metric Tons and in AIR.

If converting from VACUUM to AIR do not subtract 1.1 from Dens15/15, always use Table 56 (Dens15 is in Kg/m3, therefore 1.1, and not 0.0011)

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Definition of terms used

API Gravity API Gravity is a numerical system used on petroleum and petroleum products correlated to density and relative

density (see API MPMS Chapter 9). The relative density to API relation is: API Gravity @ 60F = (141.5 divided by relative density @ 60°F/60°F less 131.5

Automatic Sampler An automatic sampler is a device used for obtaining, by automatic means, representative sample from the fluid flowing in a pipe.

Crude Oil Washing (COW) The use of a high-pressure stream of the crude oil cargo to dislodge or dissolve clingage from the bulkheads, bottom and internal tank structures of a vessel during discharge operation.

Density The ratio of the mass of a substance to its volume. Since density is dependent on temperature and pressure these should be stated.

Free Water (FW) The water that exists in a layer. It typically lies beneath the oil.

Gross Observed Volume (GOV) Total Observed Volume (TOV) less Free Water (FW)

Gross Standard Volume (GSV) The Gross Observed Volume (GOV) multiplied by the Volume Correction Factor (VCF). This may be either the volume in a tank or correction Factor (VCF). This may be either the volume in a tank or thedifference between the volumes before and after a transfer.

Load On Top (LOT) The procedure of commingling the recovered oil slops with the next cargo by loading the cargo on top of theslops.

Meter Factor (MF) The ratio of the actual volume of liquid passed through a meter to the volume indicated by the meter.

Net Standard Volume (NSV) The Gross Standard Volume (GSV) less Sediment and Water (S+W).

Observed Reference Height Observed reference height is the distance actually measured from the tank bottom or datum plate to the established reference point.

On Board Quantity (OBQ) All Material in vessel’s cargo tanks and associated lines immediately prior to loading. OBQ quantity may include any combination of water. oil, LOT slops, oil residue, oil/water emulsions and non-liquid material.

Outturn Loss The difference in Net Standard Volume NSV between the quantity shown on the Bill of Lading and the quantity shown on the Outturn.

Reference Height Reference height is the distance from the tank bottom and/or datum plate to the established referencepoint or mark.

Remaining On Board (ROB) All material in vessel's cargo tanks and associated lines after discharge. excluding vapour. ROB may include any combination of water, oil, oil residue, oil/water emulsion and non-liquid material.

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Sediment and Water (S & W) The non-hydrocarbon solid material and water in suspension within the oil.

Sediment Suspended non-hydrocarbon solids material present within the oil but not in solution.

Slops Material collected after such operations as stripping, tank washing or dirty ballast separation. It may include oil, free water, suspended sediment and suspended water and is usually contained in a tank or tanks permanently assigned to hold such material.

Suspended Water The water within the oil which is finely dispersed as small droplets. It may, over a period of time, either collect as free water or become dissolved water, depending on the condition of temperature and pressure prevailing.

Total Calculated Volume (TCV) The Gross Standard Volume (GSV) plus Free Water (FW)

Total Delivered Volume (TDV) Total Calculated Volume (TCV) on board before discharge less Total Calculated Volume (TCV) ROB.

Total Received Volume (TRV) Total Calculated Volume (TCV) on board after loading less Total Calculated Volume (TCV) OBQ.

Total Observed Volume (TOV) The volume of oil including total water & total sediment measured at the oil temperature and pressure prevailing.

Vessel Load Ratio (VLR) The Total Received Volume (TRV) divided by the quantity (TCV) measured by the shore loading terminal, i.e.

VLR = Vessel Total Received Volume (TRV) / Shore TCV Delivered

Vessel Discharge Ratio (VDR) The Total Delivered Volume (TOV) divided by the quantity (TCV) measured by the shore loading terminal, i.e.

VDR= Vessel Total Delivered Volume (TDV) / Shore TCV Received

Vessel’s Experience Factor - Loading (VEFL) The mean of the VLRs, over several voyages is called the Vessel’s Experience Factor at Loading (VEFL).

Vessel’s Experience Factor – Discharge (VEFD) The mean of the VDRs. over several voyages is called the Vessel’s Experience Factor at Discharge (VEFD).

Volume Correction Factor (VCF or Ctl) A factor dependent upon the oil API/Density/Relative Density and temperature which corrects oil volumes tothe standard reference temperature. In dynamic measurements this factor is known as Correction for Temperature on Liquid (Ctl)

Weight Conversion Factor (WCF) A factor, dependent on the API/Density/Relative Density, for converting volume to weight-in-air. Such factorsshall be obtained from the API-ASTM-IP Petroleum Measurement Tables.

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Estimated Time of Completion of Cargo Operation

Data & Time 8/5/2005 8:00

To Load/Discharge 134,000

Estimated Rate 2,100

Time to Go (hrs) 63.8

Time to Go (hh:mm) 63:49

Time to Go (days hh:mm) 2d. 15:49

ET Completion 8/7/2005 23:48

Convert from : 134,000

Convert to : 21,304

Bbls

Cub.m.

VOLUME Converter

Estimated Time of Completion Calculator

Convert from Bbls to Cub.m.

Convert from Cub.m. to Bbls

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Estimated Time of Completion of Cargo Operation

Cub.m. 842,835 Bbls

Cub.m./hr 13,209 Bbls/hr

Bbls

Cub.m.

VOLUME Converter

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DO NOT ENTER DATA IN THIS AREA

2 Cub.m.

1 Bbls to Cub.m.

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ASTM Tables - Volume & Weight Converter

ASTM Table Crude Oils

API @ 60°F 30.40

Temperature 100.0°

QUANTITY 866,000

BBLS @ Temp. 881,874

BBLS @ 60°F 866,000

M3 @ Temp. 140,207

M3 @ 15°C 137,625

Weight MT (in Air) 120,062

Weight LT 118,174

Convert :

US Barrels/MT : 7.335 API = 33.1

(MS Excel Version 24/11/2004)

° F ° C

API Converter

C19
Example : 1. API 31.2 2. Density 859.7 kg/m³ 3. Rel.Density 0.873 MT/m³ 4. MT/US Barrel 0.13103 5. US Barrels/MT 7.335
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ASTM Tables - Volume & Weight Converter

T.3 - Density @ 15°C 873.6 kg/m³

T.2 - Temperature 37.78°C

T. 4 - (Cub.Mtrs 15°C/Bbl 60°F) 0.15892

VCF T.6A 0.9820

Density @ Obser.Temp. 0.85632 MT/m³

WCF T.13 - (MT/Bbl) 0.13864

WCF T.11 - (LT/Bbl) 0.13646

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D O N O T E N T E R D A T A I N T H I S A R E AASTM Table Used Temp. Quantity To LOAD

1 Tab. 6A API @ 60°F 1 ° F 21 Tab. 6A API @ 60°F 1 ° F 12 Tab. 6B API @ 60°F 2 ° C 23 Tab. 54A Density @ 15°C 34 Tab. 54B Density @ 15°C 4

56

API Converter6 Rel.Density to API (Tab.21) From To1 API to Density (Tab.3)2 API to Rel.Density (Tab.3)3 Density to API (Tab.51)4 Rel.Density to API (Tab.21)5 MT/US Barrel to API (Tab.13)

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6 US Barrels/MT to API 7.335 33.1

ASTM Table 6AAPI T°F API T°F A b

30.40 100.0°F 30.5 100.0 0.0004 1.014335141

ASTM Table 6B Cor1 Cor2API T°F API T°F API<37.0

30.40 100.0°F 30.5 100.0 872.59 0.000445956

ASTM Table 54ADensity15°C T°C Density15°C T°C A b

873.6 37.78°C 874 37.75 0.0008 1.014628416

ASTM Table 54B Cor1Density15°C T°C Density15°C T°C D<770 770=< D <787.5

873.6 37.78°C 874 37.75 0 0

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D O N O T E N T E R D A T A I N T H I S A R E AQuantity To LOAD ASTM Table 6A, 6B. ASTM Table 54A, 54B.

BBLS @ 60°F API 30.40 Density 873.6BBLS @ Temp. Observed Temp. 100.0°F Observed Temp. 37.78°C BBLS @ 60°F Table API 30.5 Table Density 874M3 @ Temp. Table Temp. 100.0°F Table Temp. 37.75°C M3 @ 15°C Density @ Obs.Temp. 0.85632 Density @ Obs.Temp.Weight MT (in Air) T. 4 (m³/Bbls) 0.15892 T.52 (m³/Bbls) 0.15892

T.52 (Bbls/m³)T.6A 0.9820 T.54A, 54B

T.11 (LT/Bbls) 0.13646 T.56 (Vac to Air)T.13 (MT/Bbls) in Air 0.13864 T.56 (Air to Vac)Quantity On Board 866,000 Quantity On Board

BBLS @ Temp. 881,874 BBLS @ Temp. BBLS @ 60°F 866,000 BBLS @ 60°F M3 @ Temp. 140,207 M3 @ Temp.

M3 @ 15°C 137,625 M3 @ 15°C

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Weight MT (in Air) 120,062 Weight MT (in Vac) Weight MT (in Air)

VCF6A

0.982

Cor2 Cor2 Cor337.0=< API <48.0 48.0=< API <52.0 52.0=< API <85.0

0 0 0 0.0004459557204942 1.014270583

VCF54A

0.9816

Cor1 Cor1 Cor2 VCF787.5=< D <838.5 838.5=< D <1075 54B

0 0.0004450203959805 0.0004450204 40.95 0.9817

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D O N O T E N T E R D A T A I N T H I S A R E A

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VCF6B

0.9821

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ASTM Tables - Volume & Weght Converter rsion 24/11/2004)

QUALITY CRUDE 29.00

GRADE Arabian Heavy 100.5°F

API @60°F 29.00 VCF T.6A 0.9821

Density @15°C 881.2 kg/m³ 882.0

TEMPERATURE 100.3° 38.00°C

TEMPERATURE 37.94°C VCF T.54A 0.9818

DENSITY @15°C in Air 0.8801

QUANTITY TO LOAD 1,000,000 SPECIFIC GRAVITY 60°F 0.8816

WEIGHT MT 863,880 Density @ Obser.Temp. 0.86388

M3 @ TEMP. 1,000,000 T11 - (LT/Bbl) in Air 0.13765

BBLS @ TEMP. 6,289,810 T13 - (MT/Bbl) in Air 0.13985

BBLS @ 60°F 6,177,222 T4 - (M3/Bbl) 0.15892

ASTM Table API @60°F

ASTM Table Temp.°F

ASTM Table Density @15°C

ASTM Table Temp.°C°C°F

Used : DensityAPI

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D O N O T E N T E R D A T A I N T H I S A R E A

USED Quality USED API / Density USED Temperature USED Quantity To Load

1 CRUDE 2 API @60°F 2 Fahrenheit 31 CRUDE Dencity 881.2 1 37.94°C 12 PRODUCTS API 29.00 2 100.3°F 2

34

ASTM Table 6A VCFAPI T°F API T°F A b 6A

29.00 100.3°F 29.0 100.5 0.000439716 1.01424679052 0.9821

Observed ASTM Table 6B Cor1 Cor2API T°F API T°F API<37.0 37.0=< API <48.0

29.00 100.3°F 29.0 100.5 880.7488972 0.00044057506 0

ASTM Table 54A VCFDensity15°C T°C Density15°C T°C A b 54A

881.2 37.94°C 882 38.00 0.000789245 1.014522100257 0.9818

ASTM Table 54B Cor1Density15°C T°C Density15°C T°C D<770 770=< D <787.5 787.5=< D <838.5

881.2 37.94°C 882 38.00 0 0 0

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D O N O T E N T E R D A T A I N T H I S A R E A

USED Quantity To Load

M3 @ TempMT T.52 0.15892Bbls @ 60°F T.4 0.15892M3 @ Temp T.11 0.13765Bbls @ Temp T.13 0.13985

Cor2 Cor2 Cor3 VCF48.0=< API <52.0 52.0=< API <85.0 6B

0 0 0.00044058 1.014274632 0.9821

Cor1 Cor1 Cor2 VCF838.5=< D <1075 54B0.0004397617248 0.0004397617248 41.4 0.9817

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A.P.I. CONVERTER

API = 30.0 SG = 0.8762 SG =

API = 30.2 Density = 874.6 Density =

MT/Bbl =

Bbls/MT =

E5
ASTM T.3 (SG @ 60°F) SG=141.5 / (API + 131.5)
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A.P.I. CONVERTER

0.8762 API = 30

874.6 API = 30.2

0.13392 API = 36.1

8.382 API = 56.6

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J5
ASTM T.21 (API) API=( 141.5 / SG ) - 131.5
J9
ASTM T. 3 (Density @15°C) API=(141.4292146 / (Density / 1000)) - 131.5
J13
ASTM T.13
J17
ASTM T. 13 (MT/Bbls = 1 : Bbls/MT)
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BLENDED A.P.I.

API = ((( A - ( B / C )) * D ) + (( B / C ) * E )) / A = 29.14

A = 220,000 bbls

B = 122,978 bbls

C = 0.9794 Volume Correction Factor of Cargo loaded at First Port using Final Temperature at Second Port

D = 28.00

E = 30.00

Temp. = 106.0 ° F

Prediction of Blended A.P.I. / Temp. / Volume

Volume of Tank (100%) 30,000.0 Cub.m.

API

( °F ) @obs.temp. (%)

1st Cargo 30.0 110.0 20,000.0 66.7

2nd Cargo 28.0 90.0 9,500.0 31.7

Average : 29.4 103.6°F Total : 98.3 %

TOTAL Gross Observed Volume at Second Port

Gross Standard Volume of Cargo loaded at First Port

API of Cargo loaded at Second Port

API of Cargo loaded at First Port

Final Temperature at Second Port

Temp. Volume

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BLENDED A.P.I.

Volume Correction Factor of Cargo loaded at First Port using Final Temperature at Second Port

Prediction of Blended A.P.I. / Temp. / Volume

MT

(m3) (Bbls) (Bbls)

- 125,796 122,978 17,093

- 59,753 58,970 8,299

29,503 185,569 181,969 25,392

Volume at Second Port

Volume of Cargo loaded at First Port

Volume @obs.temp.

Volume @obs.temp.

G.S.V. @60°F

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Page 25: Cargo Mate

Do Not Enter Data In This Area

Observed ASTM Table 6A VCF

API T°F API T°F 6A

30.00 106.0°F 30.0 106.0 0.9794

API = ((( A - ( B / C )) * D ) + (( B / C ) * E )) / A = 29.14

Do Not Enter Data In This Area

Observed ASTM Table 6A VCF WCF

API T°F API T°F 6A T.13

1st Cargo 30.00 110.0°F 30.0 110.0 0.9776 0.13899 20,000.0

2nd Cargo 28.00 90.0°F 28.0 90.0 0.9869 0.14073 9,500.0

29.36 103.6°F 29.5 103.5 0.9806 0.13954

Input DATA Cargo Tank2 Volume (m3)123

Volume (m3)

Volume (%)Volume (m3)Volume (bbls)

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MT

(%) (m3) (Bbls) (Bbls)

66.7 20,000 125,796 122,978 17,093

31.7 9,500 59,753 58,970 8,299

98.3 29,503 185,569 181,969 25,392

Input DATA Cargo TankVolume (m3)

Volume Volume

@obs.temp.

Volume @obs.temp.

G.S.V. @60°F

Volume (%)Volume (m3)Volume (bbls)

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CALCULATION FOR COMMINGLED CARGO (After Loading)

(a) API (1) 38.40

(b) Temp (T1) 104.5°F

(c) GOV (1) 90,000 Bbls

(d) GSV (1) @ 60°F 88,011 Bbls

(e) API (2) 33.30

(f) Final Temp (T2) 85.3°F

(g) Total GOV 30,000 Bbls 4,769.6 Cub.m.

(k) VCF(1) at Temp(T2) 0.9874 Table 6A with (a)API(1) & (f)Temp(T2)

(m) GOV(1) at Temp(T2) 89,134 Bbls 14,171.2 Cub.m. GSV(1) / VCF(1) at Temp(T2) (m) = (d) / (k)

(n) GOV ( 2nd Parcel ) -59,134 Bbls -9,401.6 Cub.m. Total GOV - GOV(1) at Temp(T2) (n) = (g) - (m)

(w) Weighted API 48.45

Example : GOV 41077 at API 38.40 & Temp 104.5, GSV @ 60F = 40169 (Table 6A) (GOV=GBbls, GOV=NBbls)

AFTER LOADING 2ND GRADE CARGO, CHECK TEMP T2(f) & ULLAGE FOR TOTAL VOLUME CARGO (g)FOR 1ST CARGO : API & NBBLS@60F (as original 1st cargo)Basis on Final Temp T2(f) and 1st Cargo API(a), Get VCF(k) from Table 6A to find GBBls(m) from NBBls.FOR 2ND CARGO : Calculate Total Quantity GBbls(g) by Final Ullage & Final Temp T2(f)2nd Cargo Quantity in GBbls(n) = Total Quantity GBbls(g) - 1st Cargo GBbls(m) at Final Temp(T2)NBbls of 2nd Cargo use API of 2nd Cargo(e) & Final Temp(T2)FOR COMMINGLED TOTAL CARGO CALCULATION :Find Avg/Weighted API(w) and use Final Temp(T2) & use find volume from final ullage & Calculate Net Volume@60F as usual.

Example : GOV 41077 at API 38.40 & Temp 104.5, GSV @ 60F = 40169 (Table 6A) (GOV=GBbls, GOV=NBbls)

AFTER LOADING 2ND GRADE CARGO, CHECK TEMP T2(f) & ULLAGE FOR TOTAL VOLUME CARGO (g)FOR 1ST CARGO : API & NBBLS@60F (as original 1st cargo)Basis on Final Temp T2(f) and 1st Cargo API(a), Get VCF(k) from Table 6A to find GBBls(m) from NBBls.FOR 2ND CARGO : Calculate Total Quantity GBbls(g) by Final Ullage & Final Temp T2(f)2nd Cargo Quantity in GBbls(n) = Total Quantity GBbls(g) - 1st Cargo GBbls(m) at Final Temp(T2)NBbls of 2nd Cargo use API of 2nd Cargo(e) & Final Temp(T2)FOR COMMINGLED TOTAL CARGO CALCULATION :Find Avg/Weighted API(w) and use Final Temp(T2) & use find volume from final ullage & Calculate Net Volume@60F as usual.

[GOV(1) at (T2)] x API(1) + GOV(2) x API(2)Weighted API = -------------------------------------------------------------------- Total GOV

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CALCULATION FOR COMMINGLED CARGO (After Loading)

Table 6A with (a)API(1) & (f)Temp(T2)

GSV(1) / VCF(1) at Temp(T2) (m) = (d) / (k)

Total GOV - GOV(1) at Temp(T2) (n) = (g) - (m)

Do Not Enter Data In This Area

ObservedAPI T°F

38.40 104.5°F 38.40 85.3°F

Example : GOV 41077 at API 38.40 & Temp 104.5, GSV @ 60F = 40169 (Table 6A) (GOV=GBbls, GOV=NBbls)

AFTER LOADING 2ND GRADE CARGO, CHECK TEMP T2(f) & ULLAGE FOR TOTAL VOLUME CARGO (g)FOR 1ST CARGO : API & NBBLS@60F (as original 1st cargo)Basis on Final Temp T2(f) and 1st Cargo API(a), Get VCF(k) from Table 6A to find GBBls(m) from NBBls.FOR 2ND CARGO : Calculate Total Quantity GBbls(g) by Final Ullage & Final Temp T2(f)2nd Cargo Quantity in GBbls(n) = Total Quantity GBbls(g) - 1st Cargo GBbls(m) at Final Temp(T2)NBbls of 2nd Cargo use API of 2nd Cargo(e) & Final Temp(T2)FOR COMMINGLED TOTAL CARGO CALCULATION :Find Avg/Weighted API(w) and use Final Temp(T2) & use find volume from final ullage & Calculate Net Volume@60F as usual.

Example : GOV 41077 at API 38.40 & Temp 104.5, GSV @ 60F = 40169 (Table 6A) (GOV=GBbls, GOV=NBbls)

AFTER LOADING 2ND GRADE CARGO, CHECK TEMP T2(f) & ULLAGE FOR TOTAL VOLUME CARGO (g)FOR 1ST CARGO : API & NBBLS@60F (as original 1st cargo)Basis on Final Temp T2(f) and 1st Cargo API(a), Get VCF(k) from Table 6A to find GBBls(m) from NBBls.FOR 2ND CARGO : Calculate Total Quantity GBbls(g) by Final Ullage & Final Temp T2(f)2nd Cargo Quantity in GBbls(n) = Total Quantity GBbls(g) - 1st Cargo GBbls(m) at Final Temp(T2)NBbls of 2nd Cargo use API of 2nd Cargo(e) & Final Temp(T2)FOR COMMINGLED TOTAL CARGO CALCULATION :Find Avg/Weighted API(w) and use Final Temp(T2) & use find volume from final ullage & Calculate Net Volume@60F as usual.

[GOV(1) at (T2)] x API(1) + GOV(2) x API(2)Weighted API = -------------------------------------------------------------------- Total GOV

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Do Not Enter Data In This Area

ASTM Table 6A VCF GOV (1) GSV (1)API T°F 6A @60°F

38.5 104.5 0.9779 90,000 88,01138.5 85.5 0.9874 89,134

Page 30: Cargo Mate

CALCULATION FOR COMMINGLED CARGO (After Loading)

FIRST PARCEL SECOND PARCEL TOTAL COMMINGLED

a API (1) 38.40 e API (2) 33.30 f FinalTemp (T2)

b GOV (1) 41,077 f FinalTemp (T2) 85.3 F g Total GOV

c GSV(1) @ 60F 40,169

d Temp (T1) 104.5 F

k

m

n

w Weighted API = [GOV(1) at (T2)] x API(1) + GOV(2) x API(2)

Total GOV

Example : GOV 41077 at API 38.40 & Temp 104.5, GSV @ 60F = 40169 (Table 6A) (GOV=GBbls, GOV=NBbls)

AFTER LOADING 2ND GRADE CARGO, CHECK TEMP T2(f) & ULLAGE FOR TOTAL VOLUME CARGO (g)

Basis on Final Temp T2(f) and 1st Cargo API(a), Get VCF(k) from Table 6A to find GBBls(m) from NBBls.

2nd Cargo Quantity in GBBls(n) = Total Quantity GBBls(g) - 1st Cargo GBBls(m) at Final Temp(T2)

NBbls of 2nd Cargo use API of 2nd Cargo(e) & Final Temp(T2)

FOR COMMINGLED TOTAL CARGO CALCULATION:

Find Avg/Weighted API(w) and use Final Temp(T2) & use find volume from final ullage

& Calculate Net Volume@60F as usual.

Temp/AP 36.9 37.4 37.9 38.4 38.9 39.4 39.9

83.8 0.9884 0.9884 0.9883 0.9882 0.9882 0.9881 0.9880 84.3 0.9882 0.9881 0.9881 0.9880 0.9879 0.9878 0.9878 84.8 0.9880 0.9879 0.9878 0.9877 0.9877 0.9876 0.9875 85.3 0.9877 0.9876 0.9876 0.9875 0.9874 0.9873 0.9873

Enter Data in Yellow Cells All Volumes in Bbls & Temp in F

VCF(1) at Temp(T2) : (Table 6A with API(1) & Temp(T2) : By 6A, a & f )

GOV(1) at Temp(T2) = GSV(1) / VCF(1) at Temp(T2) : m = c / k

GOV ( 2nd Parcel ) = Total GOV - GOV(1) at Temp(T2) : n = g - m

FOR 1ST CARGO : API & NBBLS@60F (as original 1st cargo)

FOR 2ND CARGO : Calculate Total Quantity GBBls(g) by Final Ullage & Final Temp T2(f)

Page 31: Cargo Mate

85.8 0.9875 0.9874 0.9873 0.9872 0.9872 0.9871 0.9870 86.3 0.9872 0.9871 0.9871 0.9870 0.9869 0.9868 0.9868 86.8 0.9870 0.9869 0.9868 0.9867 0.9867 0.9866 0.9865 87.3 0.9867 0.9867 0.9866 0.9865 0.9864 0.9863 0.9863 87.8 0.9865 0.9864 0.9863 0.9863 0.9862 0.9861 0.9860 88.3 0.9863 0.9862 0.9861 0.9860 0.9859 0.9858 0.9858

Page 32: Cargo Mate

CALCULATION FOR COMMINGLED CARGO (After Loading)

TOTAL COMMINGLED

85.3 F

245,222 38,987.19 M3

0.9875

40,677 6,467.20 M3

204,545 32,519.99 M3

34.15SEE NOTES BELOW

Example : GOV 41077 at API 38.40 & Temp 104.5, GSV @ 60F = 40169 (Table 6A) (GOV=GBbls, GOV=NBbls)

All Volumes in Bbls & Temp in F

Go To Menu Go To Menu

Page 33: Cargo Mate
Page 34: Cargo Mate
Page 35: Cargo Mate

LINE DISPLACEMENT Calculation (Used Table - ASTM 6A)

Cargo : Crude Oil

A.P.I. : 31.00

Shore Temp. of Cargo : 110.0

Vessel Temp. of Cargo : 90.0

Will be Loaded on Vessel : 200,000

Order @ Obs.Temp. : 201,862

Order @ Obs.Temp. : 32,094

Order @ 60°F : 197,280

Order @ 15°C : 31,365

Order M.T. : 27,250

ORDER for Loading ORDER for Loading

This programme is designed to determine quantity of cargo to be ordered for SHORE LINE DISPLACEMENT at the end of loading where there is difference in shore temperature and ship temperature of cargo.

Usual situation for Loading on SBM at Juaymah Port, when vessel will load 2 or 3 Grade of Cargo. Before completion of 1st, 2nd and 3rd Cargo, Terminal will request to Stop loading for Line Displacement when Vessel will have in Cargo Tanks free space 200,000 bbls or More ( @ Obs.Temperature ). NOT Less, due to capacity of Shore Underwater Cargo Lines 200,000 bbls, and this volume will be pushed by ANOTHER Cargo.

Problem : Due to Shore Cargo Line is Underwater - Cargo will cool.If you order for Loading 200,000 bbls, Vessel will receive 199,100 bbls due to cooling of cargo in underwater Shore Line. As result - Short Loading.

REQUIRED : Calculate Quantity of Cargo for Ordering to Terminal in order to receive 200,000 bbls at Obs.Temperature on the Vessel.

SOLUTION : Use above programme.API : Info from TerminalShore Temperature of Cargo : info from Terminal. Vessel's Temperature of Loaded Cargo : Check Temp. of Loaded Cargo in Vessel's Cargo TanksWill be loaded on Vessel : Insert quaintity of cargo to be received, after Stoppage for Shore Line Displacement.

Example :API = 31.0Shore Temperature of Cargo = 110°FVessel's Temperature of Cargo = 90°FWill be loaded on Vessel = 200,000 bbls @90°F.

Quantity for Ordering to Terminal is 201,862 bbls

Pls Note: Volume of Shore Line Displacement Can be Different for Different SBM and Ports

Page 36: Cargo Mate

This programme is designed to determine quantity of cargo to be ordered for SHORE LINE DISPLACEMENT at the end of loading where there is difference in shore temperature and ship temperature of cargo.

Usual situation for Loading on SBM at Juaymah Port, when vessel will load 2 or 3 Grade of Cargo. Before completion of 1st, 2nd and 3rd Cargo, Terminal will request to Stop loading for Line Displacement when Vessel will have in Cargo Tanks free space 200,000 bbls or More ( @ Obs.Temperature ). NOT Less, due to capacity of Shore Underwater Cargo Lines 200,000 bbls, and this volume will be pushed by ANOTHER Cargo.

Problem : Due to Shore Cargo Line is Underwater - Cargo will cool.If you order for Loading 200,000 bbls, Vessel will receive 199,100 bbls due to cooling of cargo in underwater Shore Line. As result - Short Loading.

REQUIRED : Calculate Quantity of Cargo for Ordering to Terminal in order to receive 200,000 bbls at Obs.Temperature on the Vessel.

SOLUTION : Use above programme.API : Info from TerminalShore Temperature of Cargo : info from Terminal. Vessel's Temperature of Loaded Cargo : Check Temp. of Loaded Cargo in Vessel's Cargo TanksWill be loaded on Vessel : Insert quaintity of cargo to be received, after Stoppage for Shore Line Displacement.

Example :API = 31.0Shore Temperature of Cargo = 110°FVessel's Temperature of Cargo = 90°FWill be loaded on Vessel = 200,000 bbls @90°F.

Quantity for Ordering to Terminal is 201,862 bbls

Pls Note: Volume of Shore Line Displacement Can be Different for Different SBM and Ports

Page 37: Cargo Mate

LINE DISPLACEMENT Calculation (Used Table - ASTM 6A)

°F

°F

Bbls @ Temp. 90°F

Bbls 110.0 ° C = 230.0 ° F

Cub.m. 90.0 ° F = 32.2 ° C

Bbls

Cub.m.

M.T.

Temp.°F Temp.°C

Temperatures Convertor

This programme is designed to determine quantity of cargo to be ordered for SHORE LINE DISPLACEMENT at the end of loading where there is difference in shore temperature and ship temperature of cargo.

Usual situation for Loading on SBM at Juaymah Port, when vessel will load 2 or 3 Grade of Cargo. Before completion of 1st, 2nd and 3rd Cargo, Terminal will request to Stop loading for Line Displacement when Vessel will have in Cargo Tanks free space 200,000 bbls or More ( @ Obs.Temperature ). NOT Less, due to capacity of Shore Underwater Cargo Lines 200,000 bbls, and this volume will be pushed by ANOTHER Cargo.

Problem : Due to Shore Cargo Line is Underwater - Cargo will cool.If you order for Loading 200,000 bbls, Vessel will receive 199,100 bbls due to cooling of cargo in underwater Shore Line. As result - Short Loading.

REQUIRED : Calculate Quantity of Cargo for Ordering to Terminal in order to receive 200,000 bbls at Obs.Temperature on the Vessel.

SOLUTION : Use above programme.API : Info from TerminalShore Temperature of Cargo : info from Terminal. Vessel's Temperature of Loaded Cargo : Check Temp. of Loaded Cargo in Vessel's Cargo TanksWill be loaded on Vessel : Insert quaintity of cargo to be received, after Stoppage for Shore Line Displacement.

Example :API = 31.0Shore Temperature of Cargo = 110°FVessel's Temperature of Cargo = 90°FWill be loaded on Vessel = 200,000 bbls @90°F.

Quantity for Ordering to Terminal is 201,862 bbls

Pls Note: Volume of Shore Line Displacement Can be Different for Different SBM and Ports

Go To Menu Go To Menu

Page 38: Cargo Mate

This programme is designed to determine quantity of cargo to be ordered for SHORE LINE DISPLACEMENT at the end of loading where there is difference in shore temperature and ship temperature of cargo.

Usual situation for Loading on SBM at Juaymah Port, when vessel will load 2 or 3 Grade of Cargo. Before completion of 1st, 2nd and 3rd Cargo, Terminal will request to Stop loading for Line Displacement when Vessel will have in Cargo Tanks free space 200,000 bbls or More ( @ Obs.Temperature ). NOT Less, due to capacity of Shore Underwater Cargo Lines 200,000 bbls, and this volume will be pushed by ANOTHER Cargo.

Problem : Due to Shore Cargo Line is Underwater - Cargo will cool.If you order for Loading 200,000 bbls, Vessel will receive 199,100 bbls due to cooling of cargo in underwater Shore Line. As result - Short Loading.

REQUIRED : Calculate Quantity of Cargo for Ordering to Terminal in order to receive 200,000 bbls at Obs.Temperature on the Vessel.

SOLUTION : Use above programme.API : Info from TerminalShore Temperature of Cargo : info from Terminal. Vessel's Temperature of Loaded Cargo : Check Temp. of Loaded Cargo in Vessel's Cargo TanksWill be loaded on Vessel : Insert quaintity of cargo to be received, after Stoppage for Shore Line Displacement.

Example :API = 31.0Shore Temperature of Cargo = 110°FVessel's Temperature of Cargo = 90°FWill be loaded on Vessel = 200,000 bbls @90°F.

Quantity for Ordering to Terminal is 201,862 bbls

Pls Note: Volume of Shore Line Displacement Can be Different for Different SBM and Ports

Page 39: Cargo Mate

DO NOT ENTER DATA IN THIS AREA, LINE DISPLACEMENT CALCULATIONS

Observed ASTM Table 6A

CARGO API T°C T°F API T°F

Cargo on Shore 31.00 43.33°C 110.0°F 31.0 110.0Cargo on Vessel 31.00 32.22°C 90.0°F 31.0 90.0

1 Bbls @ Temp. 2 M3 @ Temp. 3 Bbls @ 60°F4 M.T.1 Bbls @ Temp. 90°F1 °F1 90.0

Page 40: Cargo Mate

DO NOT ENTER DATA IN THIS AREA, LINE DISPLACEMENT CALCULATIONS

VCF ASTM DensityM.T.

6A T.13 @°Temp.

0.9773 0.13813 0.84909 201,862 32,094 197,280 27,250 0.9864 0.13813 0.857 200,000 31,797 197,280 27,250

Volume @obs.temp.

(Bbls)

Volume @obs.temp.

(m3)

G.S.V. @60°F

(Bbls)

Page 41: Cargo Mate

DRAFT Converter Change of Draft due to change of Density of Sea Water

Da = Dd + (( A - B ) / B * Dd )

21.60 m. = 70 Feet 10 inch Dd = 19.00 m.

A = 1.025

21.60 m. = 70.87 Feet B = 1.035

Da = 18.82 m.

70.87 Feet = 21.60 m.

70 f. 10 inch = 21.59 m. 498 mm

Dd = 19.00 m.

A = 1.025

B = 1.035

Da = 18.80 m.

Page 42: Cargo Mate

Change of Draft due to change of Density of Sea Water

Dd + (( A - B ) / B * Dd )

Draft at Port of Departure

Density of Sea Water at Port of Departure

Density of Sea Water at Port of Arrival

Draft at Port of Arrival

Allowance for fresh water (from LL Certificate)

Draft at Port of Departure

Density of Sea Water at Port of Departure

Density of Sea Water at Port of Arrival

Draft at Port of Arrival

Go To Menu Go To Menu

Page 43: Cargo Mate

Change of Draft due to List o f Boxshaped Vessel

Breadth = 58.00 m.

q°0.25 ° 0.13 m.

0.50 ° 0.25 m.

0.75 ° 0.38 m.

1.00 ° 0.51 m.

1.25 ° 0.63 m.

1.50 ° 0.76 m.

1.75 ° 0.89 m.

2.00 ° 1.01 m.

2.25 ° 1.14 m.

2.50 ° 1.27 m.

2.75 ° 1.39 m.

3.00 ° 1.52 m.

DT (m)

d1d

a

For Boxshaped VesselID = 0.5*B*sina - (d-d*cosa)ID = 0.5*B*sina (less accurately formula)

a - Angle of Heeld - DraftB - BeamID - increase in Draft due to of Heel

(Ref. Brown's Nautical Almanac 2004 p.627)

Page 44: Cargo Mate

Change of Draft due to List o f Shipshaped Vessel

d1

d

a

For Shipshaped VesselID = 0.5*B*sina - RF or accuratelyID = 0.5*B*sina + (d - RF)*cosa - d

a - Angle of Heeld - Draft (no Angle of Heel)d1 - Draft with Angle of Heel for boxshaped vessel. d2 - Draft with Angle of HeelB - BeamID - increase in Draft due to of Heel (d2 - d)RF - Although the Rise of Floor (RF) is measured along the ship's side (distance between point R and point F along the ship side) (Ref. Brown's Nautical Almanac 2004 p.627)

d2

R

F

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Page 45: Cargo Mate

Used : 2 ONE TANK FILLING RATE

m3/cm bbls/cm

CENTIMETRE / MINUTE METER / HOUR

Loading rate ( bbls/hour) Loading rate ( bbls/hour)

10,000 15,000 20,000 25,000 30,000 10,000 15,000 20,000

1 C 10.0 63 2.6 4.0 5.3 6.6 7.9 1.59 2.38 3.18

2 C 11.1 70 2.4 3.6 4.8 6.0 7.2 1.43 2.15 2.86

3 C 11.1 70 2.4 3.6 4.8 6.0 7.2 1.43 2.15 2.86

4 C 11.1 70 2.4 3.6 4.8 6.0 7.2 1.43 2.15 2.86

5 C 10.7 67 2.5 3.7 5.0 6.2 7.4 1.49 2.23 2.97

1 W 11.6 73 2.3 3.4 4.6 5.7 6.9 1.37 2.06 2.74

2 W 14.8 93 1.8 2.7 3.6 4.5 5.4 1.07 1.61 2.15

3 W 14.8 93 1.8 2.7 3.6 4.5 5.4 1.07 1.61 2.15

4 W 14.8 93 1.8 2.7 3.6 4.5 5.4 1.07 1.61 2.15

5 W 10.4 65 2.5 3.8 5.1 6.4 7.6 1.53 2.29 3.06

SL W 3.6 23 7.4 11.0 14.7 18.4 22.1 4.42 6.62 8.83

Note : For Wings Tanks m3/cm for both tanks. (example: 1P - 5.8 m3/cm, insert for 1W - 11.6 m3/cm)Filling Rate calculated for one tank (example: Filling Rate for 1P - 7.2 cm/min @ Loading Rate 5000 m3/hr)

Tank No.

M3 Bbls

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Page 46: Cargo Mate

METER / HOUR

Loading rate ( bbls/hour)

25,000 30,000

3.97 4.77

3.58 4.30

3.58 4.30

3.58 4.30

3.71 4.46

3.43 4.11

2.69 3.22

2.69 3.22

2.69 3.22

3.82 4.59

11.04 13.25

For Wings Tanks m3/cm for both tanks. (example: 1P - 5.8 m3/cm, insert for 1W - 11.6 m3/cm)Filling Rate calculated for one tank (example: Filling Rate for 1P - 7.2 cm/min @ Loading Rate 5000 m3/hr)

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Page 47: Cargo Mate

Volume of Pipe Dimensions of Pipes

System :

Size Length Volume

Pipe : 300.0 m. 54.88 cub.m 345.2 bbls

Permited Max. Loading Rate

Max. Loading Rate

Size cub.m/hr bbls/hr

Pipe : 6.0 m/sec 6,841 43,026

Flow Rates

Note 1: The above calculations are computed from the inside diameters stated, therefore for greater accuracy the inside pipe diameters should be verified.Note 2: For calculation of Max.Loading Rate See ISGOT Ed.4 - 7.4.3 ( 7.0 m/sec ) or Vessels Specifications.

Note 1: The above calculations are computed from the inside diameters stated, therefore for greater accuracy the inside pipe diameters should be verified.Note 2: For calculation of Max.Loading Rate See ISGOT Ed.4 - 7.4.3 ( 7.0 m/sec ) or Vessels Specifications.

Page 48: Cargo Mate

Dimensions of Pipes

Nominal Size Inside Size

mm. Inch. Ø mm. Do Not Enter Data In This Area

100A 97.1 1 1

150A 151.0 Metric 2

200A 190.9 Inches 3

250A 242.0 8 4

300A 293.1 482.6 5

350A 330.2 6

400A 387.4 10 7

500A 482.6 635 8

600A 584.2 9

650A 635.0 10

700A 685.8 11

750A 12

800A 13

4"

6"

8"

10"

12"

14"

16"

20"

24"

26"

28"

30"

32"

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Page 49: Cargo Mate

Do Not Enter Data In This Area

100A 97.1

150A 151

200A 190.9

250A 242

300A 293.1

350A 330.2

400A 387.4

500A 482.6

600A 584.2

650A 635

700A 685.8

750A 0

800A 0

Page 50: Cargo Mate

CAPACITIES OF PIPELINES

Nominal InsideDia Dia

Inches Inches

2 2.067

2.5 2.469

3 3.068

4 4.026

6 6.065

8 8.071

10 10.192

12 12.090

14 13.250

16 15.250

18 17.250

20 19.250

24 23.250

Note: The above calculations are computed from the inside diameters stated, therefore for greater accuracy the inside pipe diameters should be verified.

Page 51: Cargo Mate

CAPACITIES OF PIPELINES

Imp. Gals. U.S.Gals. Litres Barrelsper per per per

Foot Foot Metre Mile

0.1451 0.1743 2.165 22

0.2071 0.2487 3.089 31

0.3198 0.3540 4.769 48

0.5507 0.6613 8.213 83

1.2500 1.5010 18.640 189

2.2130 2.6580 33.010 334

3.5290 4.2380 52.630 533

4.9660 5.9640 74.060 749

5.9640 7.1630 88.960 900

7.9010 9.4890 117.840 1192

10.1090 12.1400 150.770 1525

12.5890 15.1190 187.760 1900

18.3700 22.0620 273.990 2772

The above calculations are computed from the inside diameters stated, therefore for greater accuracy the inside pipe diameters should be verified.

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Page 52: Cargo Mate

Vessel's Name : CHELSEA

ManifoldsDeck Lines

Pu

mp

Ro

om

Ris

er

Dro

p L

ine

s

Manifolds

Bottom Lines

NOTE : Before using this program on yur's Vessel, pls check figures in column Volume (m³).

Page 53: Cargo Mate

Name of Cargo Line

### Deck Line 1 90.0 566 ### Deck Line 2 90.0 566 ### Deck Line 3 90.0 566 ### Manifold Line 1 14.2 89 ### Manifold Line 2 14.2 89 ### Manifold Line 3 14.2 89 ### Drop Line 1 1.0 6 ### Drop Line 2 1.0 6 ### Drop Line 3 1.0 6 ### Pump Room Riser 1 1.0 6 ### Pump Room Riser 2 1.0 6 ### Pump Room Riser 3 1.0 6 ### Bottom Line 1 100.0 629 ### Bottom Line 2 100.0 629

Bottom Lines ### Bottom Line 3 100.0 629

GRAND TOTAL : 618.6 3,891

Volume of Marked Lines : 345.6 2,174

Volume (m³)

Volume (bbls)

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Page 54: Cargo Mate

COT 6 C COT 5 C COT 4 C COT 3 C COT 2 C

Dro

p L

ine

s

Bottom Lines

Volume of Drop Lines are calculated for level of Cargo in C.O.Ts 98%.NOTE : Before using of this program on yur's Vessel, pls check figures in column Volume (m³).

Page 55: Cargo Mate

Name of Cargo Line

1 COT 1 C: Cargo Line 1 5.9 37

1 COT 1 C: Cargo Line 2 - -

1 COT 1 C: Cargo Line 3 1.5 10 COT 1 C 1 COT 1 C: Cargo Line 1 5.9 37

1 COT 1 C: Cargo Line 2 - -

1 COT 1 C: Cargo Line 3 1.5 10

1 COT 2 C: Cargo Line 1 16.2 102

1 COT 2 C: Cargo Line 2 2.0 12

1 COT 2 C: Cargo Line 3 16.8 106

1 COT 3 C: Cargo Line 1 27.4 172

1 COT 3 C: Cargo Line 2 26.1 164

1 COT 3 C: Cargo Line 3 30.4 191

0 COT 4 C: Cargo Line 1 29.4 185

0 COT 4 C: Cargo Line 2 21.7 137

0 COT 4 C: Cargo Line 3 22.2 140

1 COT 5 C: Cargo Line 1 24.2 152

1 COT 5 C: Cargo Line 2 26.0 164

1 COT 5 C: Cargo Line 3 21.5 135

GRAND TOTAL : 271.4 1,707

Volume of Marked Lines : 198.0 1,245

Volume (m³)

Volume (bbls)

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Page 56: Cargo Mate

Volume Converter Volume Calc

19,313.9 Cub.m. = 121,481 Bbls Trim :

Ullage :

1,800,000 bbls = 286,177 Cub.m.

Change of Volume due to Change of Temperature

A.P.I. 30.7

Volume Before 100,000 Bbls

Temp. Before 110.0 ° F

Temp. After 100.0 ° F

Volume After 99,542 Bbls

API / Bbls / °F (ASTM T. 6A)

Dens. / m³ / °C (ASTM T.54A)

Page 57: Cargo Mate

Volume Calc

2.5

11.67

4.0 m. 2.5 m. 2.0 m.

11.65 19,240.6 19,367.0

11.67 19,313.9

11.70 19,186.9 19,313.3

Trim

Ullage

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Page 58: Cargo Mate

DO NOT ENTER DATA IN THIS AREA, LINE DISPLACEMENT CALCULATIONS1 Bbls

CARGO Observed ASTM Table 6A VCF

API T°F API T°F 6ABefore Change 30.70 110.0°F 30.5 110.0 0.9775 97,750 After Change 30.70 100.0°F 30.5 100.0 0.982 97,750

Observed ASTM Table 54A VCF

Before Change Density15°C T°C Density15°C T°C 54AAfter Change 30.7 110.00°C 30 110.00 0 - After Change 30.7 100.00°C 30 100.00 0 #DIV/0!

Volume @60°F (Bbls)

Volume @15°C (Cub.m.)

Page 59: Cargo Mate

DO NOT ENTER DATA IN THIS AREA, LINE DISPLACEMENT CALCULATIONS

100,000 99,542

100,000 #DIV/0!

Volume @obs.temp

. (Bbls)

Volume @obs.temp. (Cub.m.)

Page 60: Cargo Mate

Expected Average Temperature in Tank

Temp. of Cargo loaded at First Port 30.0 °

Volume of Cargo loaded at First Port 26,000

Temp. of Cargo to load at Second Port 70.0 °

Volume of Cargo to load at Second Port 300,000

Expect. Avg. Temp. of Cargo : 66.8 °

Weighted Average temperature calculated

Enter open tank temp. ? 30.0 °

Enter close tank temp. ? 70.0 °

Enter open tank volume ? 26,000

Enter Closing tank volume ? 300,000

Weighted Avg. Receipt Tank Temp : 73.8 °

Page 61: Cargo Mate

Temperature Converter

45.0 ° C = 113.0 ° F

111.0 ° F = 43.9 ° C

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Page 62: Cargo Mate

Page 610 TABLE OF CONVERSION FACTORS Brown's 2004

CONVERSION FACTORS

All Conversion Tables revised in 2002 (used PC with numeric precision of 10 digits for mantissa and 2 digits for exponent)

Compiled by P. A. S. Markland & 1С A. G. Biscoe

UNIT Multiply by FACTOR to get UNIT Multiply by FACTOR to get UNIT

Millimetres 0.03937007874 Inches 25.4 MillimetresCentimetres 0.3937007874 Inches 2.54 CentimetresMetres 3.280839895 Feet 0.3048 MetresMetres 1.093613298 Yards 0.9144 MetresKilometres 0.6213711922 Statute Miles 1.609344 KilometresKilometres 0.5399568035 Nautical Miles 1.852 KilometresSq.Centimetres 0.15500031 Sq. Inches 6.4516 Sq. CentimetresSq. Metres 10.76391042 Sq. Feet 0.09290303997 Sq. MetresSq. Metres 1.195990046 Sq. Yards 0.8361273602 Sq. MetresHectares 2.471053814 Acres 0.4046856423 HectaresSq. Kilometres 0.3861021586 Sq. Statute Miles 2.58998811 Sq. KilometresSq. Kilometres 0.2915533496 Sq. Nautical Miles 3.429904 Sq. KilometresCu. Centimetres 0.0610237441 Cu. Inches 16.387064 Cu. CentimetresCu. Metres 35.31466672 Cu. Feet 0.02831684659 Cu. MetresCu. Metres 1.307950619 Cu. Yards 0.7645548582 Cu. MetresLitres 1.759753877 Pints 0.5682612853 LitresMillilitres 0.0351950775 Fluid Ounces 28.4130643 MillilitresGrammes 0.03527396194 Ounces 28.34952313 GrammesKilogrammes 2.204622622 Pounds 0.45359237 KilogrammesMetric Tonnes 0.9842065274 Long Tons 1.016046909 Metric TonnesMetric Tonnes 1.102311311 Short Tons 0.90718474 Metric TonnesLong Tons 1.12 Short Tons 0.8928571427 Long TonsCu. Inches 0.003604649926 Imperial Gallons 277.41945 Cu. InchesCu. Feet 6.228835072 Imperial Gallons 0.1605436632 Cu. FeetCu. Metres 219.9692347 Imperial Gallons 0.004546090282 Cu. MetresUS. Gallons 0.832674133 Imperial Gallons 1.20095 US. GallonsUS. Barrels 34.97231358 Imperial Gallons 0.02859404762 US. BarrelsLitres 0.2199692346 Imperial Gallons 4.546090282 LitresCu. Inches 0.004329004329 US. Gallons 231.0 Cu. InchesCu. Feet 7.480519484 US. Gallons 0.1336805555 Cu. FeetCu. Metres 264.1720524 US. Gallons 0.003785411783 Cu. MetresUS. Barrels 42.0 US. Gallons 0 02380952381 US. BarrelsLitres 0.2641720524 US. Gallons 3.785411783 LitresCu. Inches 0.0001030715317 US. Barrels 9701.999998 Cu. InchesCu. Feet 0.1781076067 US. Barrels 5.614583332 Cu. FeetCu. Metres 6.289810772 US. Barrels 0.1589872949 Cu. MetresLitres 0.006289810772 US. Barrels 158.9872949 LitresCu. Inches 0.016387064 Litres 61.02374409 Cu. InchesCu. Feet 28.31684659 Litres 0.03531466672 Cu. FeetCu. Metres 1000.0 Litres 0.001 Cu. MetresImperial Gallons 0.004474291731 Long Tons 223.4990609 Imperial GallonsUS. Gallons 0.003725626986 Long Tons 268.4111973 US. GallonsUS. Barrels 0.1564763334 Long Tons 6.390742793 US. BarrelsCu. Feet 0.02786962526 Long Tons 35.88135796 Cu. FeetImperial Gallons 0.004546090282 Metric Tonnes 219.9692346 Imperial GallonsUS. Gallons 0.003785411783 Metric Tonnes 264.1720524 US. GallonsUS Barrels 0.1589872949 Metric Tonnes 6.289810772 US. BarrelsKg/Sq.cm 14.22334331 Lbs/Sq.Inch 0.07030695795 Kg/Sq.cmBars (1000mb) 14.50377377 Lbs/Sq.Inch 0.06894757295 Bars (1000mb)Atmospheres 14.69594878 Lbs/Sq.Inch 0.06804596389 Atmospheresmm Hg (Mercury) 0.01933677471 Lbs/Sq.Inch 51.71493256 mm Hg (Mercury)

1.422334331 Lbs/Sq.Inch 0.70306957950.4335275042 Lbs/Sq.Inch 2.306658725

Bars 1.019716213 Kg/Sq.cm 0.980665 BarsAtmospheres 1.033227453 Kg/Sq.cm 0.9678411052 Atmospheresmm Hg 0.00135951 Kg/Sq.cm 735.5592399 mm Hg

0.1 Kg/Sq.cm 100.03048 Kg/Sq.cm 32.80839895

Atmospheres 1.01325 Bars 0.9869232667 Atmospheresmm Hg 0.001333223684 Bars 750.0616827 mm Hg

0.0980665 Bars 10.197162130.0298906692 Bars 33.45525633

mm Hg 0.001315789474 Atmospheres 760.0 mm Hg0.09678411052 Atmospheres 10.332274530.02949979689 Atmospheres 33.89853848

Force de Cheval 0.9863199 Horsepower 1.013869841 Force de ChevalKilowatts 1.341022089 Horsepower 0.7456998719 KilowattsHP 0.73549875 KW 1.359621617 HPKg/Cu.m 0.06242796058 Lbs/Cu.feet 16.01846337 Kg/Cu.mKg/Cu.m 1.685554936 Lbs/Cu.yards 0.5932764212 Kg/Cu.mTonnes/Metres 0.2999861496 Tons/feet 3.333487234 Tonnes/MetresMegajoules 0.2777777778 Kilowatt Hours 3.6 MegajoulesMetres/Second 3.280839895 Feet/second 0.3048 Metres/SecondMetres/Second 196.8503937 Feet/minute 0.00508 Metres/SecondKilometres/Hour 0.6213711922 Miles/hour 1.609344 Kilometres/HourMCTC 8.20172107 MCT 1 Inch 0.121925629 MCTCMetric Tonnes/cm 2.499884582 Tons/Inch 0.4000184677 Metric Tonnes/cm

150 Metric Tonnes/cm * 2.499884582 = 374.98 Tons/Inch * 0.4000184677 = 150 Metric Tonnes/cm

         

Metres Head H2O Metres Head H20Feet Head H2O Feet Head H2O

Metres Head H2O Metres Head H2OFeet Head H2O Feet Head H2O

Metres Head H2O Metres Head H2OFeet Head H2O Feet Head H2O

Metres Head H2O Metres Head H2OFeet Head H2O Feet Head H2O

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Page 63: Cargo Mate

UNITS Converter.

Select Category :

Select Units :

Convert From : 7.50 Kg/Sq.cm

Convert To : 7.35 Bars

Used Conversion Factor : (0.980665) from Brown's Nautical Almanac 2004

Convert From : 20.80

Metres : 20.80

Fathoms : 11.37

Feet (with decimals) : 68.24

Feet & Inches : 68 Feet 3 inch

DO NOT ENTER DATA IN THIS AREA DO NOT ENTER DATA IN THIS AREA

5 Pressure 18 1 Metres 20.80 Draft Calculation1 Area 1 Metres 20.80 20.80 m 11.37 Fathoms 68.24 Feet 68 Feet 3 inch2 Density 2 Fathoms 11.37 68 Feet3 Distance 3 Feet (with decimals) 68.24 3 inch4 Power 4 Feet & Inches 68 Feet 3 inch 38.04 m 20.80 Fathoms 124.80 Feet 124 Feet 10 inch5 Pressure 124 Feet6 Speed 10 inch7 Volume 6.34 m 3.47 Fathoms 20.80 Feet 20 Feet 10 inch8 Weight 20 Feet

CALCULATION OF CONVERTIONS FACTORS 10 inchNo. UNIT Multiply by FACTOR to get UNIT Convert 8.13 m 4.45 Fathoms 26.67 Feet 20 f. 80 inch1 Atmospheres 14.69594878000000 Lbs/Sq.Inch Atmospheres to Lbs/Sq.Inch 20 Feet 80 inch2 Atmospheres 1.03322745300000 Kg/Sq.cm Atmospheres to Kg/Sq.cm 6.10 m 20 Feet 20 Feet3 Atmospheres 1.01325000000000 Bars Atmospheres to Bars 2.03 m 6.67 80 inch4 Atmospheres 760.00000000000000 mm Hg Atmospheres to mm Hg 5 Atmospheres 10.33227453000000 Metres Head H2O Atmospheres to Metres Head H2O 6 Atmospheres 33.89853848000000 Feet Head H2O Atmospheres to Feet Head H2O 7 Bars 1.01971621300000 Kg/Sq.cm Bars to Kg/Sq.cm 8 Bars 0.98692326670000 Atmospheres Bars to Atmospheres 9 Bars 750.06168270000000 mm Hg Bars to mm Hg 10 Bars 10.19716213000000 Metres Head H2O Bars to Metres Head H2O 11 Bars 33.45525633000000 Feet Head H2O Bars to Feet Head H2O 12 Bars (1000mb) 14.50377377000000 Lbs/Sq.Inch Bars (1000mb) to Lbs/Sq.Inch 13 Feet Head H2O 0.43352750420000 Lbs/Sq.Inch Feet Head H2O to Lbs/Sq.Inch 14 Feet Head H2O 0.03048000000000 Kg/Sq.cm Feet Head H2O to Kg/Sq.cm 15 Feet Head H2O 0.02989066920000 Bars Feet Head H2O to Bars 16 Feet Head H2O 0.02949979689000 Atmospheres Feet Head H2O to Atmospheres 17 Kg/Sq.cm 14.22334331000000 Lbs/Sq.Inch Kg/Sq.cm to Lbs/Sq.Inch 18 Kg/Sq.cm 0.98066500000000 Bars Kg/Sq.cm to Bars 19 Kg/Sq.cm 0.96784110520000 Atmospheres Kg/Sq.cm to Atmospheres 20 Kg/Sq.cm 735.55923990000000 mm Hg Kg/Sq.cm to mm Hg 21 Kg/Sq.cm 10.00000000000000 Metres Head H2O Kg/Sq.cm to Metres Head H2O 22 Kg/Sq.cm 32.80839895000000 Feet Head H2O Kg/Sq.cm to Feet Head H2O 23 Lbs/Sq.Inch 0.07030695795000 Kg/Sq.cm Lbs/Sq.Inch to Kg/Sq.cm 24 Lbs/Sq.Inch 0.06894757295000 Bars (1000mb) Lbs/Sq.Inch to Bars (1000mb) 25 Lbs/Sq.Inch 0.06804596389000 Atmospheres Lbs/Sq.Inch to Atmospheres 26 Lbs/Sq.Inch 51.71493256000000 mm Hg (Mercury) Lbs/Sq.Inch to mm Hg (Mercury) 27 Lbs/Sq.Inch 0.70306957950000 Metres Head H20 Lbs/Sq.Inch to Metres Head H20 28 Lbs/Sq.Inch 2.30665872500000 Feet Head H2O Lbs/Sq.Inch to Feet Head H2O 29 Metres Head H2O 1.42233433100000 Lbs/Sq.Inch Metres Head H2O to Lbs/Sq.Inch 30 Metres Head H2O 0.10000000000000 Kg/Sq.cm Metres Head H2O to Kg/Sq.cm 31 Metres Head H2O 0.09806650000000 Bars Metres Head H2O to Bars 32 Metres Head H2O 0.09678411052000 Atmospheres Metres Head H2O to Atmospheres 33 mm Hg 0.00135951000000 Kg/Sq.cm mm Hg to Kg/Sq.cm 34 mm Hg 0.00133322368400 Bars mm Hg to Bars 35 mm Hg 0.00131578947400 Atmospheres mm Hg to Atmospheres 36 mm Hg (Mercury) 0.01933677471000 Lbs/Sq.Inch mm Hg (Mercury) to Lbs/Sq.Inch

- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -

No. UNIT Multiply by FACTOR to get UNIT ConvertFrom To

- Sq. Centimetres 0.15500031 Sq. Inches Sq. Centimetres to Sq. Inches - Sq. Feet 0.09290303997 Sq. Metres Sq. Feet to Sq. Metres - Sq. Inches 6.4516 Sq. Centimetres Sq. Inches to Sq. Centimetres - Sq. Kilometres 0.3861021586 Sq. Statute Miles Sq. Kilometres to Sq. Statute Miles - Sq. Kilometres 0.2915533496 Sq. Nautical Miles Sq. Kilometres to Sq. Nautical Miles - Sq. Metres 10.76391042 Sq. Feet Sq. Metres to Sq. Feet - Sq. Metres 1.195990046 Sq. Yards Sq. Metres to Sq. Yards - Sq. Nautical Miles 3.429904 Sq. Kilometres Sq. Nautical Miles to Sq. Kilometres - Sq. Statute Miles 2.58998811 Sq. Kilometres Sq. Statute Miles to Sq. Kilometres - Sq. Yards 0.8361273602 Sq. Metres Sq. Yards to Sq. Metres - Kg/Cu.m 0.06242796058 Lbs/Cu.feet Kg/Cu.m to Lbs/Cu.feet - Kg/Cu.m 1.685554936 Lbs/Cu.yards Kg/Cu.m to Lbs/Cu.yards - Lbs/Cu.feet 16.01846337 Kg/Cu.m Lbs/Cu.feet to Kg/Cu.m - Lbs/Cu.yards 0.5932764212 Kg/Cu.m Lbs/Cu.yards to Kg/Cu.m - Pound/Gallon 0.1198264300 Kg/Ltr Pound/Gallon to Kg/Ltr - Centimetres 0.3937007874 Inches Centimetres to Inches - Fathoms 6.0000000000 Feet Fathoms to Feet - Fathoms 1.8288000000 Metres Fathoms to Metres - Feet 0.16666666666667 Fathoms Feet to Fathoms - Feet 0.3048 Metres Feet to Metres - Inches 25.4 Millimetres Inches to Millimetres - Inches 2.54 Centimetres Inches to Centimetres - Kilometres 0.6213711922 Statute Miles Kilometres to Statute Miles - Kilometres 0.5399568035 Nautical Miles Kilometres to Nautical Miles - Metres 0.54680664916885 Fathoms Metres to Fathoms - Metres 3.280839895 Feet Metres to Feet - Metres 1.093613298 Yards Metres to Yards - Millimetres 0.03937007874 Inches Millimetres to Inches - Nautical Miles 1.852 Kilometres Nautical Miles to Kilometres - Statute Miles 1.609344 Kilometres Statute Miles to Kilometres - Yards 0.9144 Metres Yards to Metres - Force de Cheval 0.9863199 Horsepower Force de Cheval to Horsepower - Horsepower 1.013869841 Force de Cheval Horsepower to Force de Cheval - Horsepower 0.7456998719 Kilowatts Horsepower to Kilowatts - HP 0.73549875 KW HP to KW - Kilowatts 1.341022089 Horsepower Kilowatts to Horsepower - KW 1.359621617 HP KW to HP 1 Atmospheres 14.69594878 Lbs/Sq.Inch Atmospheres to Lbs/Sq.Inch 2 Atmospheres 1.033227453 Kg/Sq.cm Atmospheres to Kg/Sq.cm 3 Atmospheres 1.01325 Bars Atmospheres to Bars 4 Atmospheres 760.0 mm Hg Atmospheres to mm Hg

5 Atmospheres 10.33227453 Atmospheres to Metres Head H2O

6 Atmospheres 33.89853848 Atmospheres to Feet Head H2O

7 Bars 1.019716213 Kg/Sq.cm Bars to Kg/Sq.cm 8 Bars 0.9869232667 Atmospheres Bars to Atmospheres 9 Bars 750.0616827 mm Hg Bars to mm Hg

10 Bars 10.19716213 Bars to Metres Head H2O

11 Bars 33.45525633 Bars to Feet Head H2O

12 Bars (1000mb) 14.50377377 Lbs/Sq.Inch Bars (1000mb) to Lbs/Sq.Inch

13 0.4335275042 Lbs/Sq.Inch Feet Head H2O to Lbs/Sq.Inch

14 0.03048 Kg/Sq.cm Feet Head H2O to Kg/Sq.cm

15 0.0298906692 Bars Feet Head H2O to Bars

16 0.02949979689 Atmospheres Feet Head H2O to Atmospheres

17 Kg/Sq.cm 14.22334331 Lbs/Sq.Inch Kg/Sq.cm to Lbs/Sq.Inch 18 Kg/Sq.cm 0.980665 Bars Kg/Sq.cm to Bars 19 Kg/Sq.cm 0.9678411052 Atmospheres Kg/Sq.cm to Atmospheres 20 Kg/Sq.cm 735.5592399 mm Hg Kg/Sq.cm to mm Hg

21 Kg/Sq.cm 10 Kg/Sq.cm to Metres Head H2O

22 Kg/Sq.cm 32.80839895 Kg/Sq.cm to Feet Head H2O

23 Lbs/Sq.Inch 0.07030695795 Kg/Sq.cm Lbs/Sq.Inch to Kg/Sq.cm 24 Lbs/Sq.Inch 0.06894757295 Bars (1000mb) Lbs/Sq.Inch to Bars (1000mb) 25 Lbs/Sq.Inch 0.06804596389 Atmospheres Lbs/Sq.Inch to Atmospheres 26 Lbs/Sq.Inch 51.71493256 mm Hg (Mercury) Lbs/Sq.Inch to mm Hg (Mercury)

27 Lbs/Sq.Inch 0.7030695795 Lbs/Sq.Inch to Metres Head H20

28 Lbs/Sq.Inch 2.306658725 Lbs/Sq.Inch to Feet Head H2O

29 1.422334331 Lbs/Sq.Inch Metres Head H2O to Lbs/Sq.Inch

30 0.1 Kg/Sq.cm Metres Head H2O to Kg/Sq.cm

31 0.0980665 Bars Metres Head H2O to Bars

32 0.09678411052 Atmospheres Metres Head H2O to Atmospheres

33 mm Hg 0.00135951 Kg/Sq.cm mm Hg to Kg/Sq.cm 34 mm Hg 0.001333223684 Bars mm Hg to Bars 35 mm Hg 0.001315789474 Atmospheres mm Hg to Atmospheres 36 mm Hg (Mercury) 0.01933677471 Lbs/Sq.Inch mm Hg (Mercury) to Lbs/Sq.Inch - Feet/minute 0.00508 Metres/Second Feet/minute to Metres/Second - Feet/second 0.3048 Metres/Second Feet/second to Metres/Second - Kilometres/Hour 0.6213711922 Miles/hour Kilometres/Hour to Miles/hour - Metres/Second 3.280839895 Feet/second Metres/Second to Feet/second - Metres/Second 196.8503937 Feet/minute Metres/Second to Feet/minute - Miles/hour 1.609344 Kilometres/Hour Miles/hour to Kilometres/Hour - Cu. Centimetres 0.0610237441 Cu. Inches Cu. Centimetres to Cu. Inches - Cu. Feet 6.228835072 Imperial Gallons Cu. Feet to Imperial Gallons - Cu. Feet 7.480519484 US. Gallons Cu. Feet to US. Gallons - Cu. Feet 0.1781076067 US. Barrels Cu. Feet to US. Barrels - Cu. Feet 28.31684659 Litres Cu. Feet to Litres - Cu. Feet 0.02831684659 Cu. Metres Cu. Feet to Cu. Metres - Cu. Inches 0.003604649926 Imperial Gallons Cu. Inches to Imperial Gallons - Cu. Inches 0.004329004329 US. Gallons Cu. Inches to US. Gallons - Cu. Inches 0.0001030715317 US. Barrels Cu. Inches to US. Barrels - Cu. Inches 0.016387064 Litres Cu. Inches to Litres - Cu. Inches 16.387064 Cu. Centimetres Cu. Inches to Cu. Centimetres - Cu. Metres 35.31466672 Cu. Feet Cu. Metres to Cu. Feet - Cu. Metres 1.307950619 Cu. Yards Cu. Metres to Cu. Yards - Cu. Metres 219.9692347 Imperial Gallons Cu. Metres to Imperial Gallons - Cu. Metres 264.1720524 US. Gallons Cu. Metres to US. Gallons - Cu. Metres 6.289810772 US. Barrels Cu. Metres to US. Barrels - Cu. Metres 1000.0 Litres Cu. Metres to Litres - Cu. Yards 0.7645548582 Cu. Metres Cu. Yards to Cu. Metres - Fluid Ounces 28.4130643 Millilitres Fluid Ounces to Millilitres - Imperial Gallons 277.41945 Cu. Inches Imperial Gallons to Cu. Inches - Imperial Gallons 0.1605436632 Cu. Feet Imperial Gallons to Cu. Feet - Imperial Gallons 0.004546090282 Cu. Metres Imperial Gallons to Cu. Metres - Imperial Gallons 1.20095 US. Gallons Imperial Gallons to US. Gallons - Imperial Gallons 0.02859404762 US. Barrels Imperial Gallons to US. Barrels - Imperial Gallons 4.546090282 Litres Imperial Gallons to Litres - Litres 1.759753877 Pints Litres to Pints - Litres 0.2199692346 Imperial Gallons Litres to Imperial Gallons - Litres 0.2641720524 US. Gallons Litres to US. Gallons - Litres 0.006289810772 US. Barrels Litres to US. Barrels - Litres 61.02374409 Cu. Inches Litres to Cu. Inches - Litres 0.03531466672 Cu. Feet Litres to Cu. Feet - Litres 0.001 Cu. Metres Litres to Cu. Metres - Millilitres 0.0351950775 Fluid Ounces Millilitres to Fluid Ounces - Pints 0.5682612853 Litres Pints to Litres - US. Barrels 34.97231358 Imperial Gallons US. Barrels to Imperial Gallons - US. Barrels 42.0 US. Gallons US. Barrels to US. Gallons - US. Barrels 9701.999998 Cu. Inches US. Barrels to Cu. Inches - US. Barrels 5.614583332 Cu. Feet US. Barrels to Cu. Feet - US. Barrels 0.1589872949 Cu. Metres US. Barrels to Cu. Metres - US. Barrels 158.9872949 Litres US. Barrels to Litres - US. Gallons 0.832674133 Imperial Gallons US. Gallons to Imperial Gallons - US. Gallons 231.0 Cu. Inches US. Gallons to Cu. Inches - US. Gallons 0.1336805555 Cu. Feet US. Gallons to Cu. Feet - US. Gallons 0.003785411783 Cu. Metres US. Gallons to Cu. Metres - US. Gallons 0.02380952381 US. Barrels US. Gallons to US. Barrels - US. Gallons 3.785411783 Litres US. Gallons to Litres - Grammes 0.03527396194 Ounces Grammes to Ounces - Kilogrammes 2.204622622 Pounds Kilogrammes to Pounds - Long Tons 1.12 Short Tons Long Tons to Short Tons - Long Tons 1.016046909 Metric Tonnes Long Tons to Metric Tonnes - Long Tons 223.4990609 Imperial Gallons Long Tons to Imperial Gallons - Metric Tonnes 0.9842065274 Long Tons Metric Tonnes to Long Tons - Metric Tonnes 1.102311311 Short Tons Metric Tonnes to Short Tons - Ounces 28.34952313 Grammes Ounces to Grammes - Pounds 0.45359237 Kilogrammes Pounds to Kilogrammes - Short Tons 0.90718474 Metric Tonnes Short Tons to Metric Tonnes - Short Tons 0.8928571427 Long Tons Short Tons to Long Tons

     

Metres Head H2O

Feet Head H2O

Metres Head H2O

Feet Head H2O

Feet Head H2O

Feet Head H2O

Feet Head H2O

Feet Head H2O

Metres Head H2O

Feet Head H2O

Metres Head H20

Feet Head H2O

Metres Head H2O

Metres Head H2O

Metres Head H2O

Metres Head H2O

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Page 64: Cargo Mate

Table 1

Interrelation of Units of Measurement ASTM—IP

LENGTH VOLUME AND CAPACITY *

To Convert Multiply By To Convert Multiply By

Metres: U.S. Gallons:

To Yards 1.0936 To Cubic Inches

To Feet 3.2808 To Cubic Feet 0.133681

To Inches 39.37 To Imperial Gallons 0.832674

To US Barrels 0.0238095

To Litres 3.78541

Yards: U.S. Barrels:

To Metres To US Gallons

To Cubic Inches

Feet: To Cubic Feet 5.61458

To Metres To Imperial Gallons 34.9723

To Litres 158.987

Inches: Imperial Gallons:

To Centimetres To Cubic Inches 277.42

WEIGHTTo Cubic Feet 0.160544

To US Gallons 1.20095

To US Barrels 0.0285941

To Convert Multiply ByTo Litres 4.54596 (4.54609)

Cubic Feet:

Long Tons: To Imperial Gallons 6.22883

To Pounds (Avoirdupois) To US Gallons 7.48052

To Short Tons To US Barrels 0.178108

To Metric Tons (Tonnes) 1.01605 To Litres 28.3169

To Cubic Metres 0.0283169

Cubic Inches:

Short Tons: To Imperial Gallons 0.00360465

To Pounds (Avoirdupois) To US Gallons 0.004329

To Long Tons 0.892857 To Litres 0.0163871

To Metric Tons (Tonnes) 0.907185 Litres:

To Cubic Inches 61.0238

Metric Tons (Tonnes): To Cubic Feet 0.0353147

To Long Tons 0.984206 To Imperial Gallons 0.219969

To Short Tons 1.10231 To US Gallons 0.264172

To US Barrels 0.00628981

Pounds (Avoirdupois): Cubic Metres:

To Kilograms 0.453592 To Imperial Gallons 219.969

To US Gallons 264.172

Kilograms: To US Barrels 6.28981

To Pounds (Avoirdupois) 2.20462 To Cubic Feet 35.3147

ASTM D 1250-80

231 †

0.9144 † 42 †

9702 †

0.3048 †

2.54 †

2240. †

1.12 †

2000 †

* These factors are solely for conversion at the same temperature. † This relationship is exact by definition.

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Page 65: Cargo Mate

VOLUME XI Entry With API Gravity

ASTM Tab. 3Relative Density (60/60°F) = 141.5 / ( API + 131.5 )

30.10 0.8756

ASTM Tab. 4

ASTM Tab. 8

30.000 7.296

ASTM Tab. 11LT/BBL = 0.98421*(1.01605*(22.12362536/(API+131.502609)-0.0001927941766))

29.00 0.13765

LT/BBL = 0.0375 * (( 589.9438 / ( API + 131.5 )) - 0.0050789 )

29.00 0.13765

LT/BBL = ( 589.943 / (API + 131.5) - 0.0050789 ) * 0.0375

29.00 0.13765

LT/BBL = ( ( ( 141.5 / ( API + 131.5 ) * 4.169215 ) - 0.0050789 ) * 0.0374996 )

29.00 0.13765LT/BBL = ( ЦЕЛОЕ ( 0.0375 * ( ( 589.943 / ( API + 131.5 ) ) - 0.0050789 ) * 10 ^ 5 + 0.5 ) / 10 ^ 5 , 5 )

API (60°F)

ASTM T.3 Relative Density

(60/60°F)

API (60°F)

ASTM T.4 Litres/US Gallon

API (60°F)

ASTM T.8 Pounds/US Gallon

(60°F)

API (60°F)

ASTM T.11 LT/Barrel

(60°F)

API (60°F)

ASTM T.11 LT/Barrel

(60°F)

API (60°F)

ASTM T.11 LT/Barrel

(60°F)

API (60°F)

ASTM T.11 LT/Barrel

(60°F)

Page 66: Cargo Mate

29.00 0.13765LT/BBL = ОКРУГЛ ( ( 0.168043765194 - 0.00000138081421532 * API ) / ( 1 + 0.00760520852876 * API ),5)

SGS

29.00 0.13765LT/BBL = ОКРУГЛ ( 22.12362536 / ( API + 131.502609) - 0.0001927941766, 5 )

29.00 0.13765

29.00 0.13765

LT/BBL = ( 1 / ( 5.9509641 + ( 0.0453147 * API ) )

Note: error with API=29.0

29.00 0.13764

ASTM Tab. 12BBLS/LT = 1 / ( 0.0375 * (( 589.9438 / ( API + 131.5 )) - 0.0050789 ))

30.00 7.31029

ASTM Tab. 13MT/BBL =( ( ( ( 141.5 / ( API + 131.5 ) * 4.169215 ) - 0.0050789 ) * 0.0374996 ) * 1.01605)

29.00 0.13985

MT/BBL = ОКРУГЛ ( 1 / ( 5.9506 + ( 0.0453378 * API ) ) * 1.016045 , 5 )

29.00 0.13985

API (60°F)

ASTM T.11 LT/Barrel

(60°F)

API (60°F)

ASTM T.11 LT/Barrel

(60°F)

API (60°F)

ASTM T.11 LT/Barrel

(60°F)

API (60°F)

ASTM T.11 LT/Barrel

(60°F)

API (60°F)

ASTM T.11 LT/Barrel

(60°F)

API (60°F)

ASTM T.12 Bbls/LT

(60°F)

API (60°F)

ASTM T.13 MT/Barrel

(60°F)

API (60°F)

ASTM T.13 MT/Barrel

(60°F)

Page 67: Cargo Mate

MT/BBL = (( 535.1911 / ( API + 131.5 )) - 0.0046189 ) * 0.042

Note: error with API=29.0

29.00 0.13986

MT/BBL = 1.01605 * ( 22.12362536 / ( API + 131.502609 ) - 0.0001927941766 )

Note: error with API=29.0

29.00 0.13986MT/BBL = ОКРУГЛ ( ( ЦЕЛОЕ ( 0.042 * ( ( 535.1911 / ( API + 131.5 ) ) - 0.0046189 ) * 10 ^ 5 + 0.5 ) / 10 ^ 5 ) , 5 )

Note: error with API=29.0

29.00 0.13986

Note: error with API=29.0

29.00 0.13986 0.13986

API (60°F)

ASTM T.13 MT/Barrel

(60°F)

API (60°F)

ASTM T.13 MT/Barrel

(60°F)

API (60°F)

ASTM T.13 MT/Barrel

(60°F)

API (60°F)

ASTM T.13 MT/Barrel

(60°F)

Page 68: Cargo Mate

VOLUME XI Entry With API Gravity

ASTM Tab. 3Density (15°C) = 141.4292146/(API+131.5)*1000

30.2 874.6

ASTM Tab. 4

33.00 0.15892

ASTM Tab. 8

ASTM Tab. 11LT/BBL = 0.98421*(1.01605*(22.12362536/(API+131.502609)-0.0001927941766))

LT/BBL = 0.0375 * (( 589.9438 / ( API + 131.5 )) - 0.0050789 )

LT/BBL = ( 589.943 / (API + 131.5) - 0.0050789 ) * 0.0375

LT/BBL = ( ( ( 141.5 / ( API + 131.5 ) * 4.169215 ) - 0.0050789 ) * 0.0374996 )

LT/BBL = ( ЦЕЛОЕ ( 0.0375 * ( ( 589.943 / ( API + 131.5 ) ) - 0.0050789 ) * 10 ^ 5 + 0.5 ) / 10 ^ 5 , 5 )

API (60°F)

ASTM T.3 Density

(15°C)

API (60°F)

ASTM T.4 Cub.Mtrs/Barrel

API (60°F)

Go To Menu Go To Menu

Page 69: Cargo Mate

LT/BBL = ОКРУГЛ ( ( 0.168043765194 - 0.00000138081421532 * API ) / ( 1 + 0.00760520852876 * API ),5)

LT/BBL = ОКРУГЛ ( 22.12362536 / ( API + 131.502609) - 0.0001927941766, 5 )

Note: error with API=29.0

ASTM Tab. 12BBLS/LT = 1 / ( 0.0375 * (( 589.9438 / ( API + 131.5 )) - 0.0050789 ))

ASTM Tab. 13MT/BBL =( ( ( ( 141.5 / ( API + 131.5 ) * 4.169215 ) - 0.0050789 ) * 0.0374996 ) * 1.01605)

MT/BBL = ОКРУГЛ ( 1 / ( 5.9506 + ( 0.0453378 * API ) ) * 1.016045 , 5 )

Page 70: Cargo Mate

MT/BBL = (( 535.1911 / ( API + 131.5 )) - 0.0046189 ) * 0.042

Note: error with API=29.0

MT/BBL = 1.01605 * ( 22.12362536 / ( API + 131.502609 ) - 0.0001927941766 )

Note: error with API=29.0

MT/BBL = ОКРУГЛ ( ( ЦЕЛОЕ ( 0.042 * ( ( 535.1911 / ( API + 131.5 ) ) - 0.0046189 ) * 10 ^ 5 + 0.5 ) / 10 ^ 5 ) , 5 )

Note: error with API=29.0

Note: error with API=29.0

Page 71: Cargo Mate

VOLUME XII Entry With RELATIVE DENSITY and DENSITY

ASTM Tab. 21

0.843 36.35

ASTM Tab. 29

ASTM Tab. 51API = ( 141.4292146 / D ) - 131.5

0.8450 35.87

ASTM Tab. 52Bbls @60°F Cubic to Metres @15°C

870.3 0.15892

0.6594 0.99835

879.0 877.9

MT (in Air) = ROUND((MT(in Vac) * (INT((1.0001506-(0.0012202/Density))*10000)+0.5)/10000),3)

API = ( 141.5 / Relative Density (60/60°F) ) - 131.5

Relative Density (60/60°F)

ASTM T.21 API

(60°F)

Relative Density (60/60°F)

ASTM T.29 L.Tons/1000 US Gallons (60°F)

Density (15°C)

ASTM T.51 API (60°F)

Density (15°C)

ASTM T.52 Cub.Mtr/Bbls

ASTM Tab. 56 If converting from vacuum to air do not subtract 1.1 from Dens15/15,

always use Table 56 (Dens15 is in Kg/m3, therefore 1.1, and not 0.0011)

Density at 15°C (kg/L)

ASTM T.56 Factor for

Converting Weight in Vacuo to Weight in Air

Density (15°C)

ASTM T.56 Kg/Cubic Mtr

Page 72: Cargo Mate

MT (in Air) = ОКРУГЛ((MT(in Vac) * (ЦЕЛОЕ((1.0001506-(0.0012202/Density))*10000)+0.5)/10000),3)

MT in Vacuo MT in Air

1000.0 0.6595 998.350

Density at 15°C (kg/L)

Page 73: Cargo Mate

VOLUME XII Entry With RELATIVE DENSITY and DENSITY

ASTM Tab. 21

ASTM Tab. 29

0.808 0.12614

ASTM Tab. 51

ASTM Tab. 52Cubic Metres @15°C to Bbls @60°F

853.0 6.293

0.6982 1.00155

879.0 1.1391

MT (in Air) = ROUND((MT(in Vac) * (INT((1.0001506-(0.0012202/Density))*10000)+0.5)/10000),3)

Density (15°C) = RD(60/60°F) * 999.012 / VCF(T54)

Relative Density (60/60°F)

ASTM T.21 Density

(15°C)

LT/Bbls = ( 0.0375 * ( 4.169215 * Relative Density(60/60°F) - 0.0050789 ) )

Relative Density (60/60°F)

ASTM T.29 Long Tons/Bbls

(60°F)

Relative Density (60/60°F) =

Density (15°C)

ASTM T.51 Relative Density

(60/60°F)

Density (15°C)

ASTM T.52 Bbls/Cub.Mtr

ASTM Tab. 56 If converting from vacuum to air do not subtract 1.1 from Dens15/15,

always use Table 56 (Dens15 is in Kg/m3, therefore 1.1, and not 0.0011)

Density at 15°C (kg/L)

ASTM T.56 Factor for

Converting Weight in Air to

Weight in Vacuo

Density (15°C)

ASTM T.56 Cubic Mtr/MT

Go To Menu Go To Menu

Page 74: Cargo Mate

MT (in Air) = ОКРУГЛ((MT(in Vac) * (ЦЕЛОЕ((1.0001506-(0.0012202/Density))*10000)+0.5)/10000),3)

Page 75: Cargo Mate

ASTM Tab. 6

VCF T.6 = 1 + ( h * e ) + ( s * e * e )h = f * 0.929328621 + g + ( f / 141.5 ) * APIs = ( 0.929328621 * -0.00000049 ) + 0.0000006 + ( -0.00000049 / 141.5 ) * APIe = T°F - 60

f g

API > 10.0 API <= 25.7 -0.0003948 0.00003

API > 25.7 API <= 30.2 -0.000512 0.00016

API > 30.2 API <= 35.0 -0.000617 0.00028

API > 35.0 API <= 39.0 -0.000719 0.0004

API > 39.0 API <= 43.2 -0.000843 0.00055

API > 43.2 API <= 47.6 -0.000965 0.0007

API > 47.6 API <= 52.3 -0.001084 0.00085

You Can Copy this Block in to your Programs and start work.ASTM Table 6

API T°F API T°F f g48.00 111.0°F 48.0 111.0 -0.001084 0.00085

Page 76: Cargo Mate

ASTM Tab. 6

( 0.929328621 * -0.00000049 ) + 0.0000006 + ( -0.00000049 / 141.5 ) * API

You Can Copy this Block in to your Programs and start work.VCF

h s e 6-0.00052511 -2.159E-08 51.0 0.9732

Go To Menu Go To Menu

Page 77: Cargo Mate

ASTM Tab. 6A

VCF T.6A = EXP( A * ( T°F - 60 ) * b * - 1 )

A = 341.0957 / ( 141.5 * 999.012 / ( API + 131.5 )) ^ 2b = 1 + 0.8 * A * ( T°F - 60 )

VCF T.6A = EXP ( -Y * ( 1 + 0.8 * Y ))X = ( 141.5 * 999.012 ) / ( API + 131.5 )Y = ( 341.0957 / X ^ 2 ) * ( T°F - 60 )

You Can Copy this Block in to your Programs and start work.ASTM Table 6A VCF

API T°F API T°F A b 6A38.40 85.3°F 38.5 85.5 0.0004933099 1.0100635 0.9874

You Can Copy this Block in to your Programs and start work.ASTM Table 6A VCF

API T°F API T°F X Y 6A31.20 111.0°F 31.0 111.0 869.90891077 0.0229879 0.9769

API Observed Volume

Gravity Temperature Correction

Factor

60°F °F °C Table 6A

Page 78: Cargo Mate

You Can Copy this Block in to your ProgramsASTM Table 6A VCF

API T°F API T°F 6A31.20 111.0°F 31.0 111.0 0.9769

You Can Copy this Block in to your ProgramsASTM Table 6A VCF

API T°F API T°F 6A31.20 111.0°F 31.0 111.0 0.9769

Go To Menu Go To Menu

Page 79: Cargo Mate

ASTM Tab. 6B

VCF T.6B = EXP ( Cor2 * (T°F - 60 ) * Cor3 * -1)

Cor1 = ( 141.5 * 999.012 ) / (API + 131.5 )

API < 37.0 Cor2 = ( 103.872 / Cor1 ^ 2 ) + ( 0.2701 / Cor1 )API >= 37.0 API < 48.0 Cor2 = 330.301 / Cor1 ^ 2API >= 48.0 API < 52.0 Cor2 = ( 1489.067 / Cor1 ^ 2 ) - 0.0018684API >= 52.0 API < 85.0 Cor2 = ( 192.4571 / Cor1 ^ 2 ) + ( 0.2438 / Cor1 )

Cor3 = 1 + 0.8 * Cor2 * (T°F - 60 )

You Can Copy this Block in to your Programs and start work.ASTM Table 6B Cor1 Cor2

API T°F API T°F API<37.0 37.0=< API <48.031.20 110.3°F 31.0 110.5 869.90891 0.00044775 0

API Observed Volume

Gravity Temperature Correction

Factor

60°F °F °C Table 6B

Page 80: Cargo Mate

ASTM Tab. 6B

You Can Copy this Block in to your Programs and start work.Cor2 Cor2 Cor3 VCF48.0=< API <52.0 52.0=< API <85.0 6B

0 0 0.00044775 1.018089 0.9772

Go To Menu Go To Menu

Page 81: Cargo Mate

ASTM Tab. 54A

VCF T.54A = EXP( A * b * ( T°C - 15 ) * - 1 )A = 613.9723 / Density ^ 2b = 1 + 0.8 * A * ( T°C - 15 )

You Can Copy this Block in to your Programs and start work.ASTM Table 54A

Density15°C T°C Density15°C T°C A875.7 32.70°C 876 32.75 0.0008000932

You Can Copy this Block in to your Programs and start work.ASTM Table 54A

Density15°C T°C Density15°C T°C 875.7 32.70°C 876 32.75

Density Observed Volume

Temperature Correction

Factor

15°C °F °C Table 54A

0.8757 90.86 32.70 0.9857

Page 82: Cargo Mate

ASTM Tab. 54A

You Can Copy this Block in to your Programs and start work.VCF

b 54A1.0113613231 0.9857

You Can Copy this Block in to your Programs and start work.VCF54A

0.9857

0.876

Go To Menu Go To Menu

Page 83: Cargo Mate

32.75

Page 84: Cargo Mate

ASTM Tab. 54B

VCF T.54B = EXP ( -1 * Cor1 * Cor2 * ( 1 + 0.8 * Cor1 * Cor2 ))

D < 770.0 Cor1 = ( 192.4571 / D ^ 2 ) + ( 0.2438 / D )D >= 770.0 D < 787.5 Cor1 = ( 1489.0671 / (D ^ 2)) - 0.0018684D >= 787.5 D < 838.5 Cor1 = 330.301 / D ^ 2D >= 838.5 D < 1075.0 Cor1 = ( 0.2701 / D ) + ( 103.873 / D ^2 )

Cor2 = (( T°C + 40 ) * 1.8 ) - 99

You Can Copy this Block in to your Programs and start work.

ASTM Table 54B Cor1Density15°C T°C Density15°C T°C D<770 770=< D <787.5

811 32.70°C 810 32.75 0 0

0.9770 38.9 978 39 24 346.4228

Page 85: Cargo Mate

ASTM Tab. 54B

EXP ( -1 * Cor1 * Cor2 * ( 1 + 0.8 * Cor1 * Cor2 ))

You Can Copy this Block in to your Programs and start work.

Cor1 Cor1 Cor2 VCF787.5=< D <838.5 838.5=< D <1075 54B

0.0005034308794 0 0.000503 31.95 0.9838

0.4388 0 ### ### 0 ### 0 0

Go To Menu Go To Menu

Page 86: Cargo Mate

### 0.486200 ### 0.9833 0.9833 0.00081085 0.9804

Page 87: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 87

ASTM Table 4 ASTM Table 4 ASTM Table 11

API

0.0 0.15893 0.0 3.7841 0.0 0.1680415.2 0.15893 5.6 3.7841 0.1 0.1679215.3 0.15892 5.7 3.7840 0.2 0.1677933.1 0.15892 13.5 3.7840 0.3 0.1676633.2 0.15891 13.6 3.7839 0.4 0.1675345.5 0.15891 21.1 3.7839 0.5 0.1674145.6 0.15890 21.2 3.7838 0.6 0.1672849.8 0.15890 28.6 3.7838 0.7 0.1671549.9 0.15889 28.7 3.7837 0.8 0.1670352.6 0.15889 35.9 3.7837 0.9 0.1669052.7 0.15888 36.0 3.7836 1.0 0.1667764.3 0.15888 41.0 3.7836 1.1 0.1666564.4 0.15887 41.1 3.7835 1.2 0.1665275.5 0.15887 45.6 3.7835 1.3 0.1664075.6 0.15886 45.7 3.7834 1.4 0.1662785.0 0.15886 48.4 3.7834 1.5 0.16615

48.5 3.7833 1.6 0.1660249.4 3.7833 1.7 0.1659049.5 3.7832 1.8 0.1657750.4 3.7832 1.9 0.1656550.5 3.7831 2.0 0.1655251.4 3.7831 2.1 0.1654051.5 3.7830 2.2 0.1652753.9 3.7830 2.3 0.1651554.0 3.7829 2.4 0.1650358.8 3.7829 2.5 0.1649058.9 3.7828 2.6 0.1647863.7 3.7828 2.7 0.1646663.8 3.7827 2.8 0.1645468.5 3.7827 2.9 0.1644168.6 3.7826 3.0 0.1642973.2 3.7826 3.1 0.1641773.3 3.7825 3.2 0.1640577.8 3.7825 3.3 0.1639277.9 3.7824 3.4 0.1638082.4 3.7824 3.5 0.1636882.5 3.7823 3.6 0.1635685.0 3.7823 3.7 0.16344

3.8 0.163323.9 0.163204.0 0.163084.1 0.162964.2 0.162844.3 0.162724.4 0.162604.5 0.162484.6 0.16236

API @60°F

M³ @15°C / BBL @60°F

API @60°F

Ltrs @15°C / US Gallon @60°F

LT per Bbls

Page 88: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 88

4.7 0.162244.8 0.162124.9 0.162005.0 0.161885.1 0.161765.2 0.161645.3 0.161535.4 0.161415.5 0.161295.6 0.161175.7 0.161055.8 0.160945.9 0.160826.0 0.160706.1 0.160596.2 0.160476.3 0.160356.4 0.160246.5 0.160126.6 0.160006.7 0.159896.8 0.159776.9 0.159667.0 0.159547.1 0.159437.2 0.159317.3 0.159207.4 0.159087.5 0.158977.6 0.158857.7 0.158747.8 0.158627.9 0.158518.0 0.158408.1 0.158288.2 0.158178.3 0.158068.4 0.157948.5 0.157838.6 0.157728.7 0.157608.8 0.157498.9 0.157389.0 0.157279.1 0.157159.2 0.157049.3 0.156939.4 0.156829.5 0.156719.6 0.156609.7 0.156499.8 0.156389.9 0.15626

10.0 0.15615

Page 89: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 89

10.1 0.1560410.2 0.1559310.3 0.1558210.4 0.1557110.5 0.1556010.6 0.1554910.7 0.1553810.8 0.1552710.9 0.1551711.0 0.1550611.1 0.1549511.2 0.1548411.3 0.1547311.4 0.1546211.5 0.1545111.6 0.1544111.7 0.1543011.8 0.1541911.9 0.1540812.0 0.1539712.1 0.1538712.2 0.1537612.3 0.1536512.4 0.1535512.5 0.1534412.6 0.1533312.7 0.1532312.8 0.1531212.9 0.1530113.0 0.1529113.1 0.1528013.2 0.1527013.3 0.1525913.4 0.1524913.5 0.1523813.6 0.1522713.7 0.1521713.8 0.1520713.9 0.1519614.0 0.1518614.1 0.1517514.2 0.1516514.3 0.1515414.4 0.1514414.5 0.1513414.6 0.1512314.7 0.1511314.8 0.1510214.9 0.1509215.0 0.1508215.1 0.1507115.2 0.1506115.3 0.1505115.4 0.15041

Page 90: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 90

15.5 0.1503015.6 0.1502015.7 0.1501015.8 0.1500015.9 0.1499016.0 0.1497916.1 0.1496916.2 0.1495916.3 0.1494916.4 0.1493916.5 0.1492916.6 0.1491916.7 0.1490916.8 0.1489916.9 0.1488817.0 0.1487817.1 0.1486817.2 0.1485817.3 0.1484817.4 0.1483817.5 0.1482817.6 0.1481817.7 0.1480917.8 0.1479917.9 0.1478918.0 0.1477918.1 0.1476918.2 0.1475918.3 0.1474918.4 0.1473918.5 0.1472918.6 0.1472018.7 0.1471018.8 0.1470018.9 0.1469019.0 0.1468019.1 0.1467119.2 0.1466119.3 0.1465119.4 0.1464119.5 0.1463219.6 0.1462219.7 0.1461219.8 0.1460319.9 0.1459320.0 0.1458320.1 0.1457420.2 0.1456420.3 0.1455520.4 0.1454520.5 0.1453520.6 0.1452620.7 0.1451620.8 0.14507

Page 91: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 91

20.9 0.1449721.0 0.1448821.1 0.1447821.2 0.1446921.3 0.1445921.4 0.1445021.5 0.1444021.6 0.1443121.7 0.1442121.8 0.1441221.9 0.1440322.0 0.1439322.1 0.1438422.2 0.1437422.3 0.1436522.4 0.1435622.5 0.1434622.6 0.1433722.7 0.1432822.8 0.1431822.9 0.1430923.0 0.1430023.1 0.1429123.2 0.1428123.3 0.1427223.4 0.1426323.5 0.1425423.6 0.1424423.7 0.1423523.8 0.1422623.9 0.1421724.0 0.1420824.1 0.1419924.2 0.1419024.3 0.1418024.4 0.1417124.5 0.1416224.6 0.1415324.7 0.1414424.8 0.1413524.9 0.1412625.0 0.1411725.1 0.1410825.2 0.1409925.3 0.1409025.4 0.1408125.5 0.1407225.6 0.1406325.7 0.1405425.8 0.1404525.9 0.1403626.0 0.1402726.1 0.1401826.2 0.14009

Page 92: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 92

26.3 0.1400026.4 0.1399226.5 0.1398326.6 0.1397426.7 0.1396526.8 0.1395626.9 0.1394727.0 0.1393927.1 0.1393027.2 0.1392127.3 0.1391227.4 0.1390327.5 0.1389527.6 0.1388627.7 0.1387727.8 0.1386827.9 0.1386028.0 0.1385128.1 0.1384228.2 0.1383428.3 0.1382528.4 0.1381628.5 0.1380828.6 0.1379928.7 0.1379028.8 0.1378228.9 0.1377329.0 0.1376529.1 0.1375629.2 0.1374729.3 0.1373929.4 0.1373029.5 0.1372229.6 0.1371329.7 0.1370529.8 0.1369629.9 0.1368830.0 0.1367930.1 0.1367130.2 0.1366230.3 0.1365430.4 0.1364530.5 0.1363730.6 0.1362930.7 0.1362030.8 0.1361230.9 0.1360331.0 0.1359531.1 0.1358731.2 0.1357831.3 0.1357031.4 0.1356231.5 0.1355331.6 0.13545

Page 93: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 93

31.7 0.1353731.8 0.1352831.9 0.1352032.0 0.1351232.1 0.1350332.2 0.1349532.3 0.1348732.4 0.1347932.5 0.1347032.6 0.1346232.7 0.1345432.8 0.1344632.9 0.1343833.0 0.1342933.1 0.1342133.2 0.1341333.3 0.1340533.4 0.1339733.5 0.1338933.6 0.1338133.7 0.1337233.8 0.1336433.9 0.1335634.0 0.1334834.1 0.1334034.2 0.1333234.3 0.1332434.4 0.1331634.5 0.1330834.6 0.1330034.7 0.1329234.8 0.1328434.9 0.1327635.0 0.1326835.1 0.1326035.2 0.1325235.3 0.1324435.4 0.1323635.5 0.1322835.6 0.1322035.7 0.1321235.8 0.1320435.9 0.1319636.0 0.1318936.1 0.1318136.2 0.1317336.3 0.1316536.4 0.1315736.5 0.1314936.6 0.1314136.7 0.1313436.8 0.1312636.9 0.1311837.0 0.13110

Page 94: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 94

37.1 0.1310237.2 0.1309537.3 0.1308737.4 0.1307937.5 0.1307137.6 0.1306437.7 0.1305637.8 0.1304837.9 0.1304038.0 0.1303338.1 0.1302538.2 0.1301738.3 0.1301038.4 0.1300238.5 0.1299438.6 0.1298738.7 0.1297938.8 0.1297138.9 0.1296439.0 0.1295639.1 0.1294939.2 0.1294139.3 0.1293339.4 0.1292639.5 0.1291839.6 0.1291139.7 0.1290339.8 0.1289639.9 0.1288840.0 0.1288140.1 0.1287340.2 0.1286540.3 0.1285840.4 0.1285040.5 0.1284340.6 0.1283640.7 0.1282840.8 0.1282140.9 0.1281341.0 0.1280641.1 0.1279841.2 0.1279141.3 0.1278341.4 0.1277641.5 0.1276941.6 0.1276141.7 0.1275441.8 0.1274741.9 0.1273942.0 0.1273242.1 0.1272442.2 0.1271742.3 0.1271042.4 0.12702

Page 95: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 95

42.5 0.1269542.6 0.1268842.7 0.1268142.8 0.1267342.9 0.1266643.0 0.1265943.1 0.1265143.2 0.1264443.3 0.1263743.4 0.1263043.5 0.1262343.6 0.1261543.7 0.1260843.8 0.1260143.9 0.1259444.0 0.1258644.1 0.1257944.2 0.1257244.3 0.1256544.4 0.1255844.5 0.1255144.6 0.1254444.7 0.1253644.8 0.1252944.9 0.1252245.0 0.1251545.1 0.1250845.2 0.1250145.3 0.1249445.4 0.1248745.5 0.1248045.6 0.1247345.7 0.1246645.8 0.1245945.9 0.1245146.0 0.1244446.1 0.1243746.2 0.1243046.3 0.1242346.4 0.1241646.5 0.1240946.6 0.1240246.7 0.1239646.8 0.1238946.9 0.1238247.0 0.1237547.1 0.1236847.2 0.1236147.3 0.1235447.4 0.1234747.5 0.1234047.6 0.1233347.7 0.1232647.8 0.12319

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ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 96

47.9 0.1231248.0 0.1230648.1 0.1229948.2 0.1229248.3 0.1228548.4 0.1227848.5 0.1227148.6 0.1226548.7 0.1225848.8 0.1225148.9 0.1224449.0 0.1223749.1 0.1223149.2 0.1222449.3 0.1221749.4 0.1221049.5 0.1220349.6 0.1219749.7 0.1219049.8 0.1218349.9 0.1217750.0 0.1217050.1 0.1216350.2 0.1215650.3 0.1215050.4 0.1214350.5 0.1213650.6 0.1213050.7 0.1212350.8 0.1211650.9 0.1211051.0 0.1210351.1 0.1209651.2 0.1209051.3 0.1208351.4 0.1207651.5 0.1207051.6 0.1206351.7 0.1205751.8 0.1205051.9 0.1204452.0 0.1203752.1 0.1203052.2 0.1202452.3 0.1201752.4 0.1201152.5 0.1200452.6 0.1199852.7 0.1199152.8 0.1198552.9 0.1197853.0 0.1197253.1 0.1196553.2 0.11959

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ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 97

53.3 0.1195253.4 0.1194653.5 0.1193953.6 0.1193353.7 0.1192653.8 0.1192053.9 0.1191354.0 0.1190754.1 0.1190154.2 0.1189454.3 0.1188854.4 0.1188154.5 0.1187554.6 0.1186954.7 0.1186254.8 0.1185654.9 0.1184955.0 0.1184355.1 0.1183755.2 0.1183055.3 0.1182455.4 0.1181855.5 0.1181155.6 0.1180555.7 0.1179955.8 0.1179255.9 0.1178656.0 0.1178056.1 0.1177356.2 0.1176756.3 0.1176156.4 0.1175556.5 0.1174856.6 0.1174256.7 0.1173656.8 0.1173056.9 0.1172357.0 0.1171757.1 0.1171157.2 0.1170557.3 0.1169957.4 0.1169257.5 0.1168657.6 0.1168057.7 0.1167457.8 0.1166857.9 0.1166158.0 0.1165558.1 0.1164958.2 0.1164358.3 0.1163758.4 0.1163158.5 0.1162458.6 0.11618

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ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 98

58.7 0.1161258.8 0.1160658.9 0.1160059.0 0.1159459.1 0.1158859.2 0.1158259.3 0.1157659.4 0.1157059.5 0.1156459.6 0.1155759.7 0.1155159.8 0.1154559.9 0.1153960.0 0.1153360.1 0.1152760.2 0.1152160.3 0.1151560.4 0.1150960.5 0.1150360.6 0.1149760.7 0.1149160.8 0.1148560.9 0.1147961.0 0.1147361.1 0.1146761.2 0.1146161.3 0.1145561.4 0.1144961.5 0.1144461.6 0.1143861.7 0.1143261.8 0.1142661.9 0.1142062.0 0.1141462.1 0.1140862.2 0.1140262.3 0.1139662.4 0.1139062.5 0.1138462.6 0.1137962.7 0.1137362.8 0.1136762.9 0.1136163.0 0.1135563.1 0.1134963.2 0.1134363.3 0.1133863.4 0.1133263.5 0.1132663.6 0.1132063.7 0.1131463.8 0.1130963.9 0.1130364.0 0.11297

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ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 99

64.1 0.1129164.2 0.1128564.3 0.1128064.4 0.1127464.5 0.1126864.6 0.1126264.7 0.1125764.8 0.1125164.9 0.1124565.0 0.1123965.1 0.1123465.2 0.1122865.3 0.1122265.4 0.1121665.5 0.1121165.6 0.1120565.7 0.1119965.8 0.1119465.9 0.1118866.0 0.1118266.1 0.1117766.2 0.1117166.3 0.1116566.4 0.1116066.5 0.1115466.6 0.1114866.7 0.1114366.8 0.1113766.9 0.1113267.0 0.1112667.1 0.1112067.2 0.1111567.3 0.1110967.4 0.1110367.5 0.1109867.6 0.1109267.7 0.1108767.8 0.1108167.9 0.1107668.0 0.1107068.1 0.1106468.2 0.1105968.3 0.1105368.4 0.1104868.5 0.1104268.6 0.1103768.7 0.1103168.8 0.1102668.9 0.1102069.0 0.1101569.1 0.1100969.2 0.1100469.3 0.1099869.4 0.10993

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ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 100

69.5 0.1098769.6 0.1098269.7 0.1097669.8 0.1097169.9 0.1096570.0 0.1096070.1 0.1095570.2 0.1094970.3 0.1094470.4 0.1093870.5 0.1093370.6 0.1092770.7 0.1092270.8 0.1091770.9 0.1091171.0 0.1090671.1 0.1090071.2 0.1089571.3 0.1089071.4 0.1088471.5 0.1087971.6 0.1087371.7 0.1086871.8 0.1086371.9 0.1085772.0 0.1085272.1 0.1084772.2 0.1084172.3 0.1083672.4 0.1083172.5 0.1082572.6 0.1082072.7 0.1081572.8 0.1081072.9 0.1080473.0 0.1079973.1 0.1079473.2 0.1078873.3 0.1078373.4 0.1077873.5 0.1077373.6 0.1076773.7 0.1076273.8 0.1075773.9 0.1075274.0 0.1074674.1 0.1074174.2 0.1073674.3 0.1073174.4 0.1072574.5 0.1072074.6 0.1071574.7 0.1071074.8 0.10705

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ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 101

74.9 0.1069975.0 0.1069475.1 0.1068975.2 0.1068475.3 0.1067975.4 0.1067375.5 0.1066875.6 0.1066375.7 0.1065875.8 0.1065375.9 0.1064876.0 0.1064376.1 0.1063776.2 0.1063276.3 0.1062776.4 0.1062276.5 0.1061776.6 0.1061276.7 0.1060776.8 0.1060276.9 0.1059677.0 0.1059177.1 0.1058677.2 0.1058177.3 0.1057677.4 0.1057177.5 0.1056677.6 0.1056177.7 0.1055677.8 0.1055177.9 0.1054678.0 0.1054178.1 0.1053678.2 0.1053178.3 0.1052678.4 0.1052178.5 0.1051678.6 0.1051178.7 0.1050678.8 0.1050178.9 0.1049679.0 0.1049179.1 0.1048679.2 0.1048179.3 0.1047679.4 0.1047179.5 0.1046679.6 0.1046179.7 0.1045679.8 0.1045179.9 0.1044680.0 0.1044180.1 0.1043680.2 0.10431

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Ñòðàíèöà 102

80.3 0.1042680.4 0.1042180.5 0.1041680.6 0.1041180.7 0.1040680.8 0.1040180.9 0.1039781.0 0.1039281.1 0.1038781.2 0.1038281.3 0.1037781.4 0.1037281.5 0.1036781.6 0.1036281.7 0.1035781.8 0.1035381.9 0.1034882.0 0.1034382.1 0.1033882.2 0.1033382.3 0.1032882.4 0.1032482.5 0.1031982.6 0.1031482.7 0.1030982.8 0.1030482.9 0.1029983.0 0.1029583.1 0.1029083.2 0.1028583.3 0.1028083.4 0.1027583.5 0.1027183.6 0.1026683.7 0.1026183.8 0.1025683.9 0.1025184.0 0.1024784.1 0.1024284.2 0.1023784.3 0.1023284.4 0.1022884.5 0.1022384.6 0.1021884.7 0.1021384.8 0.1020984.9 0.1020485.0 0.10199

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Ñòðàíèöà 103

ASTM Table 13 ASTM Table 22 ASTM Table 22

API

0.0 0.17074 0.656 0.15886 0.654 3.78230.1 0.17061 0.683 0.15886 0.661 3.78230.2 0.17048 0.684 0.15887 0.662 3.78240.3 0.17035 0.722 0.15887 0.675 3.78240.4 0.17022 0.723 0.15888 0.676 3.78250.5 0.17009 0.768 0.15888 0.691 3.78250.6 0.16996 0.769 0.15889 0.692 3.78260.7 0.16983 0.780 0.15889 0.707 3.78260.8 0.16971 0.781 0.15890 0.708 3.78270.9 0.16958 0.799 0.15890 0.724 3.78271.0 0.16945 0.800 0.15891 0.725 3.78281.1 0.16932 0.859 0.15891 0.743 3.78281.2 0.16919 0.860 0.15892 0.744 3.78291.3 0.16907 0.864 0.15892 0.763 3.78291.4 0.16894 0.865 0.15893 0.764 3.78301.5 0.16881 1.075 0.15893 0.773 3.78301.6 0.16869 0.774 3.78311.7 0.16856 0.777 3.78311.8 0.16843 0.778 3.78321.9 0.16831 0.781 3.78322.0 0.16818 0.782 3.78332.1 0.16805 0.786 3.78332.2 0.16793 0.787 3.78342.3 0.16780 0.798 3.78342.4 0.16768 0.799 3.78352.5 0.16755 0.820 3.78352.6 0.16743 0.821 3.78362.7 0.16730 0.844 3.78362.8 0.16718 0.845 3.78372.9 0.16705 0.883 3.78373.0 0.16693 0.884 3.78383.1 0.16680 0.926 3.78383.2 0.16668 0.927 3.78393.3 0.16656 0.975 3.78393.4 0.16643 0.976 3.78403.5 0.16631 1.031 3.78403.6 0.16618 1.032 3.78413.7 0.16606 1.075 3.78413.8 0.165943.9 0.165824.0 0.165694.1 0.165574.2 0.165454.3 0.165334.4 0.165214.5 0.165084.6 0.16496

MT per Bbls

Relative Density

( 60/60°F )

M³ @15°C / BBL @60°F

Relative Density

( 60/60°F )

Ltrs @15°C / US Gallon @60°F

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Ñòðàíèöà 104

4.7 0.164844.8 0.164724.9 0.164605.0 0.164485.1 0.164365.2 0.164245.3 0.164125.4 0.164005.5 0.163885.6 0.163765.7 0.163645.8 0.163525.9 0.163406.0 0.163286.1 0.163166.2 0.163046.3 0.162936.4 0.162816.5 0.162696.6 0.162576.7 0.162456.8 0.162346.9 0.162227.0 0.162107.1 0.161987.2 0.161877.3 0.161757.4 0.161637.5 0.161527.6 0.161407.7 0.161287.8 0.161177.9 0.161058.0 0.160948.1 0.160828.2 0.160718.3 0.160598.4 0.160488.5 0.160368.6 0.160258.7 0.160138.8 0.160028.9 0.159909.0 0.159799.1 0.159689.2 0.159569.3 0.159459.4 0.159349.5 0.159229.6 0.159119.7 0.159009.8 0.158889.9 0.15877

10.0 0.15866

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Ñòðàíèöà 105

10.1 0.1585510.2 0.1584410.3 0.1583210.4 0.1582110.5 0.1581010.6 0.1579910.7 0.1578810.8 0.1577710.9 0.1576611.0 0.1575411.1 0.1574311.2 0.1573211.3 0.1572111.4 0.1571011.5 0.1569911.6 0.1568811.7 0.1567711.8 0.1566611.9 0.1565512.0 0.1564512.1 0.1563412.2 0.1562312.3 0.1561212.4 0.1560112.5 0.1559012.6 0.1557912.7 0.1556912.8 0.1555812.9 0.1554713.0 0.1553613.1 0.1552513.2 0.1551513.3 0.1550413.4 0.1549313.5 0.1548313.6 0.1547213.7 0.1546113.8 0.1545113.9 0.1544014.0 0.1542914.1 0.1541914.2 0.1540814.3 0.1539714.4 0.1538714.5 0.1537614.6 0.1536614.7 0.1535514.8 0.1534514.9 0.1533415.0 0.1532415.1 0.1531315.2 0.1530315.3 0.1529215.4 0.15282

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Ñòðàíèöà 106

15.5 0.1527215.6 0.1526115.7 0.1525115.8 0.1524015.9 0.1523016.0 0.1522016.1 0.1520916.2 0.1519916.3 0.1518916.4 0.1517916.5 0.1516816.6 0.1515816.7 0.1514816.8 0.1513816.9 0.1512717.0 0.1511717.1 0.1510717.2 0.1509717.3 0.1508717.4 0.1507717.5 0.1506617.6 0.1505617.7 0.1504617.8 0.1503617.9 0.1502618.0 0.1501618.1 0.1500618.2 0.1499618.3 0.1498618.4 0.1497618.5 0.1496618.6 0.1495618.7 0.1494618.8 0.1493618.9 0.1492619.0 0.1491619.1 0.1490619.2 0.1489619.3 0.1488619.4 0.1487619.5 0.1486719.6 0.1485719.7 0.1484719.8 0.1483719.9 0.1482720.0 0.1481720.1 0.1480820.2 0.1479820.3 0.1478820.4 0.1477820.5 0.1476920.6 0.1475920.7 0.1474920.8 0.14740

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Ñòðàíèöà 107

20.9 0.1473021.0 0.1472021.1 0.1471021.2 0.1470121.3 0.1469121.4 0.1468221.5 0.1467221.6 0.1466221.7 0.1465321.8 0.1464321.9 0.1463422.0 0.1462422.1 0.1461522.2 0.1460522.3 0.1459622.4 0.1458622.5 0.1457722.6 0.1456722.7 0.1455822.8 0.1454822.9 0.1453923.0 0.1452923.1 0.1452023.2 0.1451123.3 0.1450123.4 0.1449223.5 0.1448223.6 0.1447323.7 0.1446423.8 0.1445423.9 0.1444524.0 0.1443624.1 0.1442624.2 0.1441724.3 0.1440824.4 0.1439924.5 0.1438924.6 0.1438024.7 0.1437124.8 0.1436224.9 0.1435325.0 0.1434325.1 0.1433425.2 0.1432525.3 0.1431625.4 0.1430725.5 0.1429825.6 0.1428925.7 0.1427925.8 0.1427025.9 0.1426126.0 0.1425226.1 0.1424326.2 0.14234

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Ñòðàíèöà 108

26.3 0.1422526.4 0.1421626.5 0.1420726.6 0.1419826.7 0.1418926.8 0.1418026.9 0.1417127.0 0.1416227.1 0.1415327.2 0.1414427.3 0.1413527.4 0.1412627.5 0.1411827.6 0.1410927.7 0.1410027.8 0.1409127.9 0.1408228.0 0.1407328.1 0.1406428.2 0.1405628.3 0.1404728.4 0.1403828.5 0.1402928.6 0.1402028.7 0.1401228.8 0.1400328.9 0.1399429.0 0.1398529.1 0.1397729.2 0.1396829.3 0.1395929.4 0.1395129.5 0.1394229.6 0.1393329.7 0.1392529.8 0.1391629.9 0.1390730.0 0.1389930.1 0.1389030.2 0.1388230.3 0.1387330.4 0.1386430.5 0.1385630.6 0.1384730.7 0.1383930.8 0.1383030.9 0.1382231.0 0.1381331.1 0.1380531.2 0.1379631.3 0.1378831.4 0.1377931.5 0.1377131.6 0.13762

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Ñòðàíèöà 109

31.7 0.1375431.8 0.1374531.9 0.1373732.0 0.1372832.1 0.1372032.2 0.1371232.3 0.1370332.4 0.1369532.5 0.1368732.6 0.1367832.7 0.1367032.8 0.1366232.9 0.1365333.0 0.1364533.1 0.1363733.2 0.1362833.3 0.1362033.4 0.1361233.5 0.1360433.6 0.1359533.7 0.1358733.8 0.1357933.9 0.1357134.0 0.1356234.1 0.1355434.2 0.1354634.3 0.1353834.4 0.1353034.5 0.1352134.6 0.1351334.7 0.1350534.8 0.1349734.9 0.1348935.0 0.1348135.1 0.1347335.2 0.1346535.3 0.1345735.4 0.1344835.5 0.1344035.6 0.1343235.7 0.1342435.8 0.1341635.9 0.1340836.0 0.1340036.1 0.1339236.2 0.1338436.3 0.1337636.4 0.1336836.5 0.1336036.6 0.1335236.7 0.1334436.8 0.1333636.9 0.1332837.0 0.13321

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Ñòðàíèöà 110

37.1 0.1331337.2 0.1330537.3 0.1329737.4 0.1328937.5 0.1328137.6 0.1327337.7 0.1326537.8 0.1325837.9 0.1325038.0 0.1324238.1 0.1323438.2 0.1322638.3 0.1321838.4 0.1321138.5 0.1320338.6 0.1319538.7 0.1318738.8 0.1318038.9 0.1317239.0 0.1316439.1 0.1315639.2 0.1314939.3 0.1314139.4 0.1313339.5 0.1312639.6 0.1311839.7 0.1311039.8 0.1310339.9 0.1309540.0 0.1308740.1 0.1308040.2 0.1307240.3 0.1306440.4 0.1305740.5 0.1304940.6 0.1304240.7 0.1303440.8 0.1302640.9 0.1301941.0 0.1301141.1 0.1300441.2 0.1299641.3 0.1298941.4 0.1298141.5 0.1297441.6 0.1296641.7 0.1295941.8 0.1295141.9 0.1294442.0 0.1293642.1 0.1292942.2 0.1292142.3 0.1291442.4 0.12906

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ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 111

42.5 0.1289942.6 0.1289142.7 0.1288442.8 0.1287742.9 0.1286943.0 0.1286243.1 0.1285443.2 0.1284743.3 0.1284043.4 0.1283243.5 0.1282543.6 0.1281843.7 0.1281043.8 0.1280343.9 0.1279644.0 0.1278844.1 0.1278144.2 0.1277444.3 0.1276744.4 0.1275944.5 0.1275244.6 0.1274544.7 0.1273844.8 0.1273044.9 0.1272345.0 0.1271645.1 0.1270945.2 0.1270145.3 0.1269445.4 0.1268745.5 0.1268045.6 0.1267345.7 0.1266645.8 0.1265845.9 0.1265146.0 0.1264446.1 0.1263746.2 0.1263046.3 0.1262346.4 0.1261646.5 0.1260946.6 0.1260146.7 0.1259446.8 0.1258746.9 0.1258047.0 0.1257347.1 0.1256647.2 0.1255947.3 0.1255247.4 0.1254547.5 0.1253847.6 0.1253147.7 0.1252447.8 0.12517

Page 112: Cargo Mate

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Ñòðàíèöà 112

47.9 0.1251048.0 0.1250348.1 0.1249648.2 0.1248948.3 0.1248248.4 0.1247548.5 0.1246848.6 0.1246148.7 0.1245448.8 0.1244848.9 0.1244149.0 0.1243449.1 0.1242749.2 0.1242049.3 0.1241349.4 0.1240649.5 0.1239949.6 0.1239249.7 0.1238649.8 0.1237949.9 0.1237250.0 0.1236550.1 0.1235850.2 0.1235150.3 0.1234550.4 0.1233850.5 0.1233150.6 0.1232450.7 0.1231750.8 0.1231150.9 0.1230451.0 0.1229751.1 0.1229051.2 0.1228451.3 0.1227751.4 0.1227051.5 0.1226451.6 0.1225751.7 0.1225051.8 0.1224351.9 0.1223752.0 0.1223052.1 0.1222352.2 0.1221752.3 0.1221052.4 0.1220352.5 0.1219752.6 0.1219052.7 0.1218452.8 0.1217752.9 0.1217053.0 0.1216453.1 0.1215753.2 0.12151

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ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 113

53.3 0.1214453.4 0.1213753.5 0.1213153.6 0.1212453.7 0.1211853.8 0.1211153.9 0.1210554.0 0.1209854.1 0.1209154.2 0.1208554.3 0.1207854.4 0.1207254.5 0.1206554.6 0.1205954.7 0.1205254.8 0.1204654.9 0.1204055.0 0.1203355.1 0.1202755.2 0.1202055.3 0.1201455.4 0.1200755.5 0.1200155.6 0.1199455.7 0.1198855.8 0.1198255.9 0.1197556.0 0.1196956.1 0.1196256.2 0.1195656.3 0.1195056.4 0.1194356.5 0.1193756.6 0.1193156.7 0.1192456.8 0.1191856.9 0.1191257.0 0.1190557.1 0.1189957.2 0.1189357.3 0.1188657.4 0.1188057.5 0.1187457.6 0.1186757.7 0.1186157.8 0.1185557.9 0.1184958.0 0.1184258.1 0.1183658.2 0.1183058.3 0.1182458.4 0.1181758.5 0.1181158.6 0.11805

Page 114: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 114

58.7 0.1179958.8 0.1179258.9 0.1178659.0 0.1178059.1 0.1177459.2 0.1176859.3 0.1176159.4 0.1175559.5 0.1174959.6 0.1174359.7 0.1173759.8 0.1173159.9 0.1172560.0 0.1171860.1 0.1171260.2 0.1170660.3 0.1170060.4 0.1169460.5 0.1168860.6 0.1168260.7 0.1167660.8 0.1167060.9 0.1166361.0 0.1165761.1 0.1165161.2 0.1164561.3 0.1163961.4 0.1163361.5 0.1162761.6 0.1162161.7 0.1161561.8 0.1160961.9 0.1160362.0 0.1159762.1 0.1159162.2 0.1158562.3 0.1157962.4 0.1157362.5 0.1156762.6 0.1156162.7 0.1155562.8 0.1154962.9 0.1154363.0 0.1153763.1 0.1153163.2 0.1152563.3 0.1152063.4 0.1151463.5 0.1150863.6 0.1150263.7 0.1149663.8 0.1149063.9 0.1148464.0 0.11478

Page 115: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 115

64.1 0.1147264.2 0.1146664.3 0.1146164.4 0.1145564.5 0.1144964.6 0.1144364.7 0.1143764.8 0.1143164.9 0.1142665.0 0.1142065.1 0.1141465.2 0.1140865.3 0.1140265.4 0.1139665.5 0.1139165.6 0.1138565.7 0.1137965.8 0.1137365.9 0.1136866.0 0.1136266.1 0.1135666.2 0.1135066.3 0.1134566.4 0.1133966.5 0.1133366.6 0.1132766.7 0.1132266.8 0.1131666.9 0.1131067.0 0.1130467.1 0.1129967.2 0.1129367.3 0.1128767.4 0.1128267.5 0.1127667.6 0.1127067.7 0.1126567.8 0.1125967.9 0.1125368.0 0.1124868.1 0.1124268.2 0.1123668.3 0.1123168.4 0.1122568.5 0.1122068.6 0.1121468.7 0.1120868.8 0.1120368.9 0.1119769.0 0.1119169.1 0.1118669.2 0.1118069.3 0.1117569.4 0.11169

Page 116: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 116

69.5 0.1116469.6 0.1115869.7 0.1115269.8 0.1114769.9 0.1114170.0 0.1113670.1 0.1113070.2 0.1112570.3 0.1111970.4 0.1111470.5 0.1110870.6 0.1110370.7 0.1109770.8 0.1109270.9 0.1108671.0 0.1108171.1 0.1107571.2 0.1107071.3 0.1106471.4 0.1105971.5 0.1105371.6 0.1104871.7 0.1104371.8 0.1103771.9 0.1103272.0 0.1102672.1 0.1102172.2 0.1101572.3 0.1101072.4 0.1100572.5 0.1099972.6 0.1099472.7 0.1098872.8 0.1098372.9 0.1097873.0 0.1097273.1 0.1096773.2 0.1096173.3 0.1095673.4 0.1095173.5 0.1094573.6 0.1094073.7 0.1093573.8 0.1092973.9 0.1092474.0 0.1091974.1 0.1091374.2 0.1090874.3 0.1090374.4 0.1089774.5 0.1089274.6 0.1088774.7 0.1088274.8 0.10876

Page 117: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 117

74.9 0.1087175.0 0.1086675.1 0.1086075.2 0.1085575.3 0.1085075.4 0.1084575.5 0.1083975.6 0.1083475.7 0.1082975.8 0.1082475.9 0.1081976.0 0.1081376.1 0.1080876.2 0.1080376.3 0.1079876.4 0.1079276.5 0.1078776.6 0.1078276.7 0.1077776.8 0.1077276.9 0.1076777.0 0.1076177.1 0.1075677.2 0.1075177.3 0.1074677.4 0.1074177.5 0.1073677.6 0.1073077.7 0.1072577.8 0.1072077.9 0.1071578.0 0.1071078.1 0.1070578.2 0.1070078.3 0.1069578.4 0.1068978.5 0.1068478.6 0.1067978.7 0.1067478.8 0.1066978.9 0.1066479.0 0.1065979.1 0.1065479.2 0.1064979.3 0.1064479.4 0.1063979.5 0.1063479.6 0.1062979.7 0.1062479.8 0.1061879.9 0.1061380.0 0.1060880.1 0.1060380.2 0.10598

Page 118: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 118

80.3 0.1059380.4 0.1058880.5 0.1058380.6 0.1057880.7 0.1057380.8 0.1056880.9 0.1056381.0 0.1055881.1 0.1055381.2 0.1054881.3 0.1054381.4 0.1053981.5 0.1053481.6 0.1052981.7 0.1052481.8 0.1051981.9 0.1051482.0 0.1050982.1 0.1050482.2 0.1049982.3 0.1049482.4 0.1048982.5 0.1048482.6 0.1047982.7 0.1047482.8 0.1047082.9 0.1046583.0 0.1046083.1 0.1045583.2 0.1045083.3 0.1044583.4 0.1044083.5 0.1043583.6 0.1043183.7 0.1042683.8 0.1042183.9 0.1041684.0 0.1041184.1 0.1040684.2 0.1040184.3 0.1039784.4 0.1039284.5 0.1038784.6 0.1038284.7 0.1037784.8 0.1037384.9 0.1036885.0 0.10363

Page 119: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 119

ASTM Table 52 ASTM Table 52 ASTM Table 56

654.0 6.295 654.0 0.15886 0.5000 0.99775697.0 6.295 683.0 0.15886 0.5191 0.99775698.0 6.294 684.0 0.15887 0.5192 0.99785778.0 6.294 722.0 0.15887 0.5421 0.99785779.0 6.293 723.0 0.15888 0.5422 0.99795901.0 6.293 768.0 0.15888 0.5673 0.99795902.0 6.292 769.0 0.15889 0.5674 0.99805

1074.0 6.292 779.0 0.15889 0.5950 0.99805780.0 0.15890 0.5951 0.99815798.0 0.15890 0.6255 0.99815799.0 0.15891 0.6256 0.99825859.0 0.15891 0.6593 0.99825860.0 0.15892 0.6594 0.99835964.0 0.15892 0.6970 0.99835965.0 0.15893 0.6971 0.99845

1074.0 0.15893 0.7392 0.998450.7393 0.998550.7869 0.998550.7870 0.998650.8411 0.998650.8412 0.998750.9034 0.998750.9035 0.998850.9756 0.998850.9757 0.998951.0604 0.998951.0605 0.999051.1000 0.99905

DENSITY @ 15°C

US Bbls @60°F / M³ @15°C

DENSITY @ 15°C

M³ @15°C / US Bbl @60°F

DENSITY @ 15°C

(kg/L)

Factor for Converting Weight in

Vacuo to Weight in Air

Page 120: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 120

ASTM Table 56 ASTM Table 57

0.5000 1.00225 0 0.00000.5201 1.00225 654 0.64260.5202 1.00215 655 0.64360.5432 1.00215 656 0.64450.5433 1.00205 657 0.64550.5684 1.00205 658 0.64650.5685 1.00195 659 0.64750.5960 1.00195 660 0.64850.5961 1.00185 661 0.64950.6265 1.00185 662 0.65040.6266 1.00175 663 0.65140.6603 1.00175 664 0.65240.6604 1.00165 665 0.65340.6980 1.00165 666 0.65440.6981 1.00155 667 0.65540.7402 1.00155 668 0.65630.7403 1.00145 669 0.65730.7879 1.00145 670 0.65830.7880 1.00135 671 0.65930.8421 1.00135 672 0.66030.8422 1.00125 673 0.66130.9044 1.00125 674 0.66230.9045 1.00115 675 0.66320.9766 1.00115 676 0.66420.9767 1.00105 677 0.66521.0614 1.00105 678 0.66621.0615 1.00095 679 0.66721.1000 1.00095 680 0.6682

681 0.6691682 0.6701683 0.6711684 0.6721685 0.6731686 0.6741687 0.6751688 0.6760689 0.6770690 0.6780691 0.6790692 0.6800693 0.6810694 0.6819695 0.6829696 0.6839697 0.6849698 0.6859699 0.6869

DENSITY @ 15°C

(kg/L)

Factor for Converting Weight in

Air to Weight in Vacuo

DENSITY @ 15°C

LT per Cub.M.

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Page 121: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 121

700 0.6878701 0.6888702 0.6898703 0.6908704 0.6918705 0.6928706 0.6938707 0.6947708 0.6957709 0.6967710 0.6977711 0.6987712 0.6997713 0.7006714 0.7016715 0.7026716 0.7036717 0.7046718 0.7056719 0.7066720 0.7075721 0.7085722 0.7095723 0.7105724 0.7115725 0.7125726 0.7134727 0.7144728 0.7154729 0.7164730 0.7174731 0.7184732 0.7193733 0.7203734 0.7213735 0.7223736 0.7233737 0.7243738 0.7253739 0.7262740 0.7272741 0.7282742 0.7292743 0.7302744 0.7312745 0.7321746 0.7331747 0.7341748 0.7351749 0.7361750 0.7371751 0.7380752 0.7390753 0.7400

Page 122: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 122

754 0.7410755 0.7420756 0.7430757 0.7440758 0.7449759 0.7459760 0.7469761 0.7479762 0.7489763 0.7499764 0.7508765 0.7518766 0.7528767 0.7538768 0.7548769 0.7558770 0.7568771 0.7577772 0.7587773 0.7597774 0.7607775 0.7617776 0.7627777 0.7636778 0.7646779 0.7656780 0.7666781 0.7676782 0.7686783 0.7695784 0.7705785 0.7715786 0.7725787 0.7735788 0.7745789 0.7755790 0.7764791 0.7774792 0.7784793 0.7794794 0.7804795 0.7814796 0.7823797 0.7833798 0.7843799 0.7853800 0.7863801 0.7873802 0.7883803 0.7892804 0.7902805 0.7912806 0.7922807 0.7932

Page 123: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 123

808 0.7942809 0.7951810 0.7961811 0.7971812 0.7981813 0.7991814 0.8001815 0.8010816 0.8020817 0.8030818 0.8040819 0.8050820 0.8060821 0.8070822 0.8079823 0.8089824 0.8099825 0.8109826 0.8119827 0.8129828 0.8138829 0.8148830 0.8158831 0.8168832 0.8178833 0.8188834 0.8198835 0.8207836 0.8217837 0.8227838 0.8237839 0.8247840 0.8257841 0.8266842 0.8276843 0.8286844 0.8296845 0.8306846 0.8316847 0.8325848 0.8335849 0.8345850 0.8355851 0.8365852 0.8375853 0.8385854 0.8394855 0.8404856 0.8414857 0.8424858 0.8434859 0.8444860 0.8453861 0.8463

Page 124: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 124

862 0.8473863 0.8483864 0.8493865 0.8503866 0.8513867 0.8522868 0.8532869 0.8542870 0.8552871 0.8562872 0.8572873 0.8581874 0.8591875 0.8601876 0.8611877 0.8621878 0.8631879 0.8640880 0.8650881 0.8660882 0.8670883 0.8680884 0.8690885 0.8700886 0.8709887 0.8719888 0.8729889 0.8739890 0.8749891 0.8759892 0.8768893 0.8778894 0.8788895 0.8798896 0.8808897 0.8818898 0.8827899 0.8837900 0.8847901 0.8857902 0.8867903 0.8877904 0.8887905 0.8896906 0.8906907 0.8916908 0.8926909 0.8936910 0.8946911 0.8955912 0.8965913 0.8975914 0.8985915 0.8995

Page 125: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 125

916 0.9005917 0.9015918 0.9024919 0.9034920 0.9044921 0.9054922 0.9064923 0.9074924 0.9083925 0.9093926 0.9103927 0.9113928 0.9123929 0.9133930 0.9142931 0.9152932 0.9162933 0.9172934 0.9182935 0.9192936 0.9202937 0.9211938 0.9221939 0.9231940 0.9241941 0.9251942 0.9261943 0.9270944 0.9280945 0.9290946 0.9300947 0.9310948 0.9320949 0.9330950 0.9339951 0.9349952 0.9359953 0.9369954 0.9379955 0.9389956 0.9398957 0.9408958 0.9418959 0.9428960 0.9438961 0.9448962 0.9457963 0.9467964 0.9477965 0.9487966 0.9497967 0.9507968 0.9517969 0.9526

Page 126: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 126

970 0.9536971 0.9546972 0.9556973 0.9566974 0.9576975 0.9585976 0.9595977 0.9605978 0.9615979 0.9625980 0.9635981 0.9645982 0.9654983 0.9664984 0.9674985 0.9684986 0.9694987 0.9704988 0.9713989 0.9723990 0.9733991 0.9743992 0.9753993 0.9763994 0.9772995 0.9782996 0.9792997 0.9802998 0.9812999 0.9822

1000 0.98321001 0.98411002 0.98511003 0.98611004 0.98711005 0.98811006 0.98911007 0.99001008 0.99101009 0.99201010 0.99301011 0.99401012 0.99501013 0.99601014 0.99691015 0.99791016 0.99891017 0.99991018 1.00091019 1.00191020 1.00281021 1.00381022 1.00481023 1.0058

Page 127: Cargo Mate

ASTM 4, 11, 13, 22, 52, 56, 57

Ñòðàíèöà 127

1024 1.00681025 1.00781026 1.00871027 1.00971028 1.01071029 1.01171030 1.01271031 1.01371032 1.01471033 1.01561034 1.01661035 1.01761036 1.01861037 1.01961038 1.02061039 1.02151040 1.02251041 1.02351042 1.02451043 1.02551044 1.02651045 1.02741046 1.02841047 1.02941048 1.03041049 1.03141050 1.03241051 1.03341052 1.03431053 1.03531054 1.03631055 1.03731056 1.03831057 1.03931058 1.04021059 1.04121060 1.04221061 1.04321062 1.04421063 1.04521064 1.04621065 1.04711066 1.04811067 1.04911068 1.05011069 1.05111070 1.05211071 1.05301072 1.05401073 1.05501074 1.05601075 1.0570

Page 128: Cargo Mate

Conversion Tables for Crude Oil

Based on ASTM Tables D1250-80 53A, 51, 56 & 58

Duplicate of Table produced and utilsed by Nafta Moscow

20° 15° API FACT

0.8200 0.8236 40.22 7.6403

0.8201 0.8237 40.20 7.6394

0.8202 0.8238 40.18 7.6385

0.8203 0.8239 40.16 7.6376

0.8204 0.8240 40.14 7.6367

0.8205 0.8241 40.12 7.6358

0.8206 0.8242 40.10 7.6349

0.8207 0.8243 40.08 7.6340

0.8208 0.8244 40.06 7.6331

0.8209 0.8245 40.04 7.6322

0.8210 0.8246 40.01 7.6313

0.8211 0.8247 39.99 7.6304

0.8212 0.8248 39.97 7.6295

0.8213 0.8249 39.95 7.6286

0.8214 0.8250 39.93 7.6277

0.8215 0.8251 39.91 7.6268

0.8216 0.8252 39.89 7.6259

0.8217 0.8253 39.87 7.6250

0.8218 0.8254 39.85 7.6241

0.8219 0.8255 39.83 7.6232

0.8220 0.8256 39.80 7.6223

0.8221 0.8257 39.78 7.6214

0.8222 0.8258 39.76 7.6205

0.8223 0.8259 39.74 7.6196

0.8224 0.8260 39.72 7.6187

0.8225 0.8261 39.70 7.6177

0.8226 0.8262 39.68 7.6167

0.8227 0.8263 39.66 7.6157

0.8228 0.8264 39.64 7.6147

0.8229 0.8265 39.62 7.6137

0.8230 0.8266 39.59 7.6127

0.8231 0.8267 39.57 7.6117

0.8232 0.8268 39.55 7.6107

0.8233 0.8269 39.53 7.6097

0.8234 0.8270 39.51 7.6087

0.8235 0.8271 39.49 7.6078

0.8236 0.8272 39.47 7.6069

0.8237 0.8273 39.45 7.6060

0.8238 0.8274 39.43 7.6051

0.8239 0.8275 39.41 7.6042

0.8240 0.8276 39.39 7.6033

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Page 129: Cargo Mate

0.8241 0.8277 39.37 7.6024

0.8242 0.8278 39.35 7.6015

0.8243 0.8279 39.33 7.6006

0.8244 0.8280 39.31 7.5997

0.8245 0.8281 39.29 7.5988

0.8246 0.8282 39.27 7.5979

0.8247 0.8283 39.25 7.5970

0.8248 0.8284 39.23 7.5961

0.8249 0.8285 39.21 7.5952

0.8250 0.8286 39.18 7.5943

0.8251 0.8287 39.16 7.5934

0.8252 0.8288 39.14 7.5925

0.8253 0.8289 39.12 7.5916

0.8254 0.8290 39.10 7.5907

0.8255 0.8291 39.08 7.5898

0.8256 0.8292 39.06 7.5889

0.8257 0.8293 39.04 7.5880

0.8258 0.8294 39.02 7.5871

0.8259 0.8295 39.00 7.5862

0.8260 0.8296 38.98 7.5853

0.8261 0.8297 38.96 7.5844

0.8262 0.8298 38.94 7.5835

0.8263 0.8299 38.92 7.5826

0.8264 0.8300 38.90 7.5818

0.8265 0.8301 38.88 7.5809

0.8266 0.8302 38.86 7.5800

0.8267 0.8303 38.84 7.5791

0.8268 0.8304 38.82 7.5782

0.8269 0.8305 38.80 7.5773

0.8270 0.8306 38.77 7.5764

0.8271 0.8307 38.75 7.5755

0.8272 0.8308 38.73 7.5746

0.8273 0.8309 38.71 7.5737

0.8274 0.8310 38.69 7.5728

0.8275 0.8311 38.67 7.5718

0.8276 0.8312 38.65 7.5708

0.8277 0.8313 38.63 7.5698

0.8278 0.8314 38.61 7.5688

0.8279 0.8315 38.59 7.5678

0.8280 0.8316 38.57 7.5668

0.8281 0.8317 38.55 7.5658

0.8282 0.8318 38.53 7.5648

0.8283 0.8319 38.51 7.5638

0.8284 0.8320 38.49 7.5628

0.8285 0.8321 38.47 7.5619

0.8286 0.8322 38.45 7.5610

Page 130: Cargo Mate

0.8287 0.8323 38.43 7.5601

0.8288 0.8324 38.41 7.5592

0.8289 0.8325 38.39 7.5583

0.8290 0.8326 38.36 7.5574

0.8291 0.8327 38.34 7.5565

0.8292 0.8328 38.32 7.5556

0.8293 0.8329 38.30 7.5547

0.8294 0.8330 38.28 7.5538

0.8295 0.8331 38.26 7.5529

0.8296 0.8332 38.24 7.5520

0.8297 0.8333 38.22 7.5511

0.8298 0.8334 38.20 7.5502

0.8299 0.8335 38.18 7.5493

0.8300 0.8336 38.16 7.5484

0.8301 0.8337 38.14 7.5475

0.8302 0.8338 38.12 7.5466

0.8303 0.8339 38.10 7.5457

0.8304 0.8340 38.08 7.5448

0.8305 0.8341 38.06 7.5439

0.8306 0.8342 38.04 7.5430

0.8307 0.8343 38.02 7.5421

0.8308 0.8344 38.00 7.5412

0.8309 0.8345 37.98 7.5403

0.8310 0.8346 37.95 7.5394

0.8311 0.8347 37.93 7.5385

0.8312 0.8348 37.91 7.5376

0.8313 0.8349 37.89 7.5367

0.8314 0.8350 37.87 7.5358

0.8315 0.8351 37.85 7.5349

0.8316 0.8352 37.83 7.5340

0.8317 0.8353 37.81 7.5331

0.8318 0.8354 37.79 7.5322

0.8319 0.8355 37.77 7.5313

0.8320 0.8356 37.75 7.5304

0.8321 0.8357 37.73 7.5295

0.8322 0.8358 37.71 7.5286

0.8323 0.8359 37.69 7.5277

0.8324 0.8360 37.67 7.5268

0.8325 0.8361 37.65 7.5259

0.8326 0.8362 37.63 7.5250

0.8327 0.8363 37.61 7.5241

0.8328 0.8364 37.59 7.5232

0.8329 0.8365 37.57 7.5223

0.8330 0.8366 37.55 7.5214

0.8331 0.8367 37.53 7.5205

0.8332 0.8368 37.51 7.5196

Page 131: Cargo Mate

0.8333 0.8369 37.49 7.5187

0.8334 0.8370 37.47 7.5178

0.8335 0.8371 37.45 7.5169

0.8336 0.8372 37.43 7.5160

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0.8380 0.8416 36.54 7.4772

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0.8426 0.8461 35.65 7.4378

0.8427 0.8462 35.63 7.4369

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0.8469 0.8504 34.80 7.4001

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0.8472 0.8507 34.75 7.3974

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0.8514 0.8549 33.93 7.3607

0.8515 0.8550 33.91 7.3598

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0.8518 0.8553 33.85 7.3574

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0.8547 0.8582 33.29 7.3322

0.8548 0.8583 33.27 7.3314

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0.8555 0.8590 33.14 7.3258

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0.8560 0.8595 33.05 7.3213

0.8561 0.8596 33.03 7.3204

0.8562 0.8597 33.01 7.3195

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0.8563 0.8598 32.99 7.3186

0.8564 0.8599 32.97 7.3177

0.8565 0.8600 32.95 7.3168

0.8566 0.8601 32.93 7.3160

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0.8654 0.8688 31.28 7.2427

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0.8655 0.8689 31.26 7.2418

0.8656 0.8690 31.24 7.2409

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0.8699 0.8733 30.44 7.2056

0.8700 0.8734 30.42 7.2048

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0.8702 0.8736 30.39 7.2032

0.8703 0.8737 30.37 7.2024

0.8704 0.8738 30.35 7.2016

0.8705 0.8739 30.33 7.2008

0.8706 0.8740 30.31 7.2000

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0.8708 0.8742 30.27 7.1982

0.8709 0.8743 30.26 7.1973

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0.8745 0.8779 29.59 7.1678

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0.8790 0.8824 28.77 7.1309

0.8791 0.8825 28.75 7.1301

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0.8794 0.8828 28.70 7.1277

0.8795 0.8829 28.68 7.1269

0.8796 0.8830 28.66 7.1261

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0.8798 0.8832 28.62 7.1245

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0.8810 0.8844 28.41 7.1149

0.8811 0.8845 28.39 7.1141

0.8812 0.8846 28.37 7.1133

0.8813 0.8847 28.35 7.1125

0.8814 0.8848 28.34 7.1117

0.8815 0.8849 28.32 7.1109

0.8816 0.8850 28.30 7.1101

0.8817 0.8851 28.28 7.1093

0.8818 0.8852 28.26 7.1085

0.8819 0.8853 28.25 7.1077

0.8820 0.8854 28.23 7.1069

0.8821 0.8855 28.21 7.1061

0.8822 0.8856 28.19 7.1053

0.8823 0.8857 28.17 7.1045

0.8824 0.8858 28.16 7.1037

0.8825 0.8859 28.14 7.1029

0.8826 0.8860 28.12 7.1021

0.8827 0.8861 28.10 7.1013

0.8828 0.8862 28.08 7.1005

0.8829 0.8863 28.07 7.0997

0.8830 0.8864 28.05 7.0989

0.8831 0.8865 28.03 7.0981

0.8832 0.8866 28.01 7.0973

0.8833 0.8867 27.99 7.0965

0.8834 0.8868 27.98 7.0957

0.8835 0.8869 27.96 7.0949

0.8836 0.8870 27.94 7.0941

0.8837 0.8871 27.92 7.0933

0.8838 0.8872 27.90 7.0925

Page 142: Cargo Mate

0.8839 0.8873 27.89 7.0917

0.8840 0.8874 27.87 7.0909

0.8841 0.8875 27.85 7.0901

0.8842 0.8876 27.83 7.0893

0.8843 0.8877 27.81 7.0885

0.8844 0.8878 27.80 7.0877

0.8845 0.8879 27.78 7.0869

0.8846 0.8880 27.76 7.0861

0.8847 0.8881 27.74 7.0853

0.8848 0.8882 27.72 7.0845

0.8849 0.8883 27.71 7.0837

0.8850 0.8884 27.69 7.0829

0.8851 0.8885 27.67 7.0821

0.8852 0.8886 27.65 7.0813

0.8853 0.8887 27.63 7.0805

0.8854 0.8888 27.62 7.0797

0.8855 0.8889 27.60 7.0789

0.8856 0.8890 27.58 7.0781

0.8857 0.8891 27.56 7.0773

0.8858 0.8892 27.54 7.0765

0.8859 0.8893 27.53 7.0757

0.8860 0.8894 27.51 7.0749

0.8861 0.8895 27.49 7.0742

0.8862 0.8896 27.47 7.0734

0.8863 0.8897 27.46 7.0727

0.8864 0.8898 27.44 7.0719

0.8865 0.8899 27.42 7.0712

0.8866 0.8900 27.41 7.0704

0.8867 0.8901 27.39 7.0696

0.8868 0.8902 27.37 7.0689

0.8869 0.8903 27.35 7.0681

0.8870 0.8904 27.34 7.0674

0.8871 0.8905 27.32 7.0666

0.8872 0.8905 27.30 7.0658

0.8873 0.8906 27.29 7.0651

0.8874 0.8907 27.27 7.0643

0.8875 0.8908 27.25 7.0636

0.8876 0.8909 27.23 7.0628

0.8877 0.8910 27.22 7.0620

0.8878 0.8911 27.20 7.0613

0.8879 0.8912 27.18 7.0605

0.8880 0.8913 27.17 7.0598

0.8881 0.8914 27.15 7.0590

0.8882 0.8915 27.13 7.0582

0.8883 0.8916 27.11 7.0574

0.8884 0.8917 27.09 7.0565

Page 143: Cargo Mate

0.8885 0.8918 27.08 7.0558

0.8886 0.8919 27.06 7.0550

0.8887 0.8920 27.04 7.0542

0.8888 0.8921 27.02 7.0534

0.8889 0.8922 27.01 7.0526

0.8890 0.8923 26.99 7.0518

0.8891 0.8924 26.97 7.0510

0.8892 0.8925 26.96 7.0502

0.8893 0.8926 26.94 7.0494

0.8894 0.8927 26.92 7.0486

0.8895 0.8928 26.90 7.0478

0.8896 0.8929 26.89 7.0470

0.8897 0.8930 26.87 7.0462

0.8898 0.8931 26.85 7.0454

0.8899 0.8932 26.83 7.0446

0.8900 0.8933 26.82 7.0438

0.8901 0.8934 26.80 7.0430

0.8902 0.8935 26.78 7.0422

0.8903 0.8936 26.76 7.0414

0.8904 0.8937 26.74 7.0406

0.8905 0.8938 26.73 7.0398

0.8906 0.8939 26.71 7.0390

0.8907 0.8940 26.69 7.0382

0.8908 0.8941 26.67 7.0374

0.8909 0.8942 26.65 7.0366

0.8910 0.8943 26.64 7.0358

0.8911 0.8944 26.62 7.0350

0.8912 0.8945 26.60 7.0342

0.8913 0.8946 26.58 7.0334

0.8914 0.8947 26.56 7.0326

0.8915 0.8948 26.55 7.0318

0.8916 0.8949 26.53 7.0310

0.8917 0.8950 26.51 7.0302

0.8918 0.8951 26.49 7.0294

0.8919 0.8952 26.48 7.0286

0.8920 0.8953 26.46 7.0278

0.8921 0.8954 26.44 7.0270

0.8922 0.8955 26.43 7.0262

0.8923 0.8956 26.41 7.0254

0.8924 0.8957 26.39 7.0246

0.8925 0.8958 26.37 7.0238

0.8926 0.8959 26.36 7.0230

0.8927 0.8960 26.34 7.0222

0.8928 0.8961 26.32 7.0215

0.8929 0.8962 26.30 7.0208

0.8930 0.8963 26.29 7.0201

Page 144: Cargo Mate

0.8931 0.8964 26.27 7.0194

0.8932 0.8965 26.25 7.0187

0.8933 0.8966 26.23 7.0180

0.8934 0.8967 26.21 7.0173

0.8935 0.8968 26.20 7.0166

0.8936 0.8969 26.18 7.0159

0.8937 0.8970 26.16 7.0152

0.8938 0.8971 26.14 7.0144

0.8939 0.8972 26.12 7.0136

0.8940 0.8973 26.11 7.0128

0.8941 0.8974 26.09 7.0120

0.8942 0.8975 26.07 7.0112

0.8943 0.8976 26.05 7.0104

0.8944 0.8977 26.03 7.0096

0.8945 0.8978 26.02 7.0088

0.8946 0.8979 26.00 7.0080

0.8947 0.8980 25.98 7.0072

0.8948 0.8981 25.96 7.0064

0.8949 0.8982 25.95 7.0056

0.8950 0.8983 25.93 7.0048

0.8951 0.8984 25.91 7.0040

0.8952 0.8985 25.89 7.0032

0.8953 0.8986 25.88 7.0024

0.8954 0.8987 25.86 7.0016

0.8955 0.8988 25.84 7.0008

0.8956 0.8989 25.83 7.0000

0.8957 0.8990 25.81 6.9992

0.8958 0.8991 25.79 6.9984

0.8959 0.8992 25.77 6.9976

0.8960 0.8993 25.76 6.9968

0.8961 0.8994 25.74 6.9960

0.8962 0.8995 25.72 6.9952

0.8963 0.8996 25.70 6.9944

0.8964 0.8997 25.68 6.9936

0.8965 0.8998 25.67 6.9928

0.8966 0.8999 25.65 6.9920

0.8967 0.9000 25.63 6.9913

0.8968 0.9001 25.61 6.9905

0.8969 0.9002 25.60 6.9897

0.8970 0.9003 25.58 6.9889

0.8971 0.9004 25.56 6.9881

0.8972 0.9005 25.54 6.9873

0.8973 0.9006 25.53 6.9865

0.8974 0.9007 25.51 6.9857

0.8975 0.9008 25.49 6.9849

0.8976 0.9009 25.48 6.9841

Page 145: Cargo Mate

0.8977 0.9010 25.46 6.9833

0.8978 0.9011 25.44 6.9826

0.8979 0.9012 25.43 6.9819

0.8980 0.9013 25.41 6.9812

0.8981 0.9014 25.39 6.9805

0.8982 0.9015 25.37 6.9798

0.8983 0.9016 25.36 6.9791

0.8984 0.9017 25.34 6.9784

0.8985 0.9018 25.32 6.9777

0.8986 0.9019 25.31 6.9770

0.8987 0.9020 25.29 6.9763

0.8988 0.9021 25.27 6.9755

0.8989 0.9022 25.25 6.9747

0.8990 0.9023 25.24 6.9739

0.8991 0.9024 25.22 6.9731

0.8992 0.9025 25.20 6.9723

0.8993 0.9026 25.18 6.9715

0.8994 0.9027 25.16 6.9707

0.8995 0.9028 25.15 6.9699

0.8996 0.9029 25.13 6.9691

0.8997 0.9030 25.11 6.9683

0.8998 0.9031 25.09 6.9675

0.8999 0.9032 25.08 6.9667

0.9000 0.9033 25.06 6.9659

0.9001 0.9034 25.04 6.9651

0.9002 0.9035 25.02 6.9650

0.9003 0.9036 25.01 6.9642

0.9004 0.9037 24.99 6.9634

0.9005 0.9038 24.97 6.9626

0.9006 0.9039 24.96 6.9618

0.9007 0.9040 24.94 6.9610

0.9008 0.9041 24.92 6.9602

0.9009 0.9042 24.91 6.9594

0.9010 0.9043 24.89 6.9586

0.9011 0.9044 24.87 6.9578

0.9012 0.9045 24.85 6.9570

0.9013 0.9046 24.84 6.9562

0.9014 0.9047 24.82 6.9554

0.9015 0.9048 24.80 6.9546

0.9016 0.9049 24.79 6.9538

0.9017 0.9050 24.77 6.9530

0.9018 0.9051 24.75 6.9523

0.9019 0.9052 24.73 6.9516

0.9020 0.9053 24.72 6.9509

0.9021 0.9054 24.70 6.9502

0.9022 0.9055 24.68 6.9495

Page 146: Cargo Mate

0.9023 0.9056 24.66 6.9488

0.9024 0.9057 24.64 6.9481

0.9025 0.9058 24.63 6.9474

0.9026 0.9059 24.61 6.9467

0.9027 0.9060 24.59 6.9460

0.9028 0.9061 24.57 6.9452

0.9029 0.9062 24.56 6.9444

0.9030 0.9063 24.54 6.9436

0.9031 0.9064 24.52 6.9428

0.9032 0.9065 24.50 6.9420

0.9033 0.9066 24.48 6.9412

0.9034 0.9067 24.47 6.9404

0.9035 0.9068 24.45 6.9396

0.9036 0.9069 24.44 6.9388

0.9037 0.9070 24.42 6.9380

0.9038 0.9071 24.40 6.9372

0.9039 0.9072 24.39 6.9364

0.9040 0.9073 24.37 6.9356

0.9041 0.9074 24.35 6.9348

0.9042 0.9075 24.33 6.9340

0.9043 0.9076 24.32 6.9332

0.9044 0.9077 24.30 6.9324

0.9045 0.9078 24.28 6.9316

0.9046 0.9079 24.27 6.9308

0.9047 0.9080 24.25 6.9300

0.9048 0.9081 24.23 6.9293

0.9049 0.9082 24.22 6.9286

0.9050 0.9083 24.20 6.9278

0.9051 0.9084 24.18 6.9272

0.9052 0.9085 24.16 6.9265

0.9053 0.9086 24.15 6.9258

Page 147: Cargo Mate

SGS WEDGE FORMULA WEDGE FORMULA

V = ( W * A² ) / ( 2 * f )Ic = ( L - Y ) * ff = T / L.B.P. A =

A = I + ( Y * f ) D =S =

Ic = U =L = Lengh of Tank W =Y = Distance from gauge point to Aft Bulkhead DF =T = Trim L =

L.B.P.= Length Between Perpendiculars F =A = Height of wedge at bulkheadI = Innage (Dip) Note : A² = { [ (U-DF) x F ] + S }² (4 dec places)

V = Volume Note : If (A) > (LxF) then do not apply Wedge FormulaW = Width of Tank

WEDGE FORMULA WEDGE FORMULA (KiL)

V= (( T * Y / L.B.P. + I )² * W * L ) / ( 2 * T )

V= Volume V =T= Trim D =Y= Distance from gauge point to Aft Bulkhead H =

L.B.P.= Length Between Perpendiculars T = I = Innage (Dip) Y =W= Width of Tank Lpp =

B =

Critical Innage (if I<Ic Wedge formula applicable)

Page 148: Cargo Mate

WEDGE FORMULA

V = ( { [ (U-DF) x F ] + S }² x W ) / 2

Adjusted innage at aft bulkhead of tankMean total gauge heightSounding (innage)Distance from ullage point to aft bulkheadWidth of tankMean gauge height x trim factorLength of tankTrim Factor ( Trim / LBP ) (4 dec)

Note : A² = { [ (U-DF) x F ] + S }² (4 dec places) Note : If (A) > (LxF) then do not apply Wedge Formula

WEDGE FORMULA (KiL)

V = ( D - (H*T²)/Lpp² + (Y*T)/Lpp )² * Lpp * B

Volume of liquid.Sounding of liquid from bottom at ullage hatch (not ullage)Height of cargo tank. From bottom plate to deck plate.Vessel's TrimDistance from measuring point to tank aft bulkhead.Length between perpendiculars.Width of cargo tank.

Go To Menu Go To Menu

Page 149: Cargo Mate

IV.1.3. Wedge formula This SAYBOLT wedge-formula is only to be used with liquid, when the liquid doesn't touch all four bulkheads.By means of soundings the innage of the liquid is determined. On this innage a correction, (different from the trim correction from the calibration tables) has to be applied. This correction is calculated using the wedge formula.

Abbreviations used:Ls =length between perpendiculars Ts = trim of the vesselY = distance from the ullage point to the aft bulkheadDa = dip corrected to aft bulkheadD = observed dipDt = total height of the tank

First the measured dip has to be corrected as it if was measured at the aft bulkhead:

Next the length of the wedge is calculated by:

If Lw is less then the length of that particular cargo tank, the wedge formula is applicable.If the wedge formula is applicable, we now enter the ship's calibration tables for that particular tank, with the following dip value:

The wedge volume can now be calculated with the following formula:

in which: V =Volume found in ships calibration tables at even keel at dip Da/2.

Example:Measured dip D = 14 cm = 0.14 meter Y = 2.00 meter ( distance from the ullage point to the aft bulkhead )Dt = 27.49 meter ( total height of the tank ) Lt = 40.00 meter ( length of the tank )Ls = 329.20 meter (length between perpendiculars )Ts = 2.50 meter (trim of the vessel)

Corrected dip:

 = 0.14 + ((2.00- 0.2088) x 0.0076) = 0.14 + (1.7912 x 0.0076) = 0.1536 m

Check is Lw less than Lt:

We now enter the ship's calibration tables at even keel at a dip of 0.1536 / 2 = 0.08 m. In a imaginairy calibration table the volume for 0.08 m even-keel is read, being 16,032 Ltr.The wedge volume can now be calculated as:

     TsDF = Dt x -----          Ls

          (Y-Df) x Ts Da= D + ----------------              Ls

    (Y-DF) x Ts  When   --------------------- is less then zero, then let Da=D.           Ls

  Ls Lw = Da x -----          Ts

Page 150: Cargo Mate

IV.1.3. Wedge formula This SAYBOLT wedge-formula is only to be used with liquid, when the liquid doesn't touch all four bulkheads.By means of soundings the innage of the liquid is determined. On this innage a correction, (different from the trim correction from the calibration tables) has to be applied. This correction is calculated using the wedge formula.

Abbreviations used:Ls =length between perpendiculars Ts = trim of the vesselY = distance from the ullage point to the aft bulkheadDa = dip corrected to aft bulkheadD = observed dipDt = total height of the tank

First the measured dip has to be corrected as it if was measured at the aft bulkhead:

Next the length of the wedge is calculated by:

If Lw is less then the length of that particular cargo tank, the wedge formula is applicable.If the wedge formula is applicable, we now enter the ship's calibration tables for that particular tank, with the following dip value:

The wedge volume can now be calculated with the following formula:

in which: V =Volume found in ships calibration tables at even keel at dip Da/2.

Example:Measured dip D = 14 cm = 0.14 meter Y = 2.00 meter ( distance from the ullage point to the aft bulkhead )Dt = 27.49 meter ( total height of the tank ) Lt = 40.00 meter ( length of the tank )Ls = 329.20 meter (length between perpendiculars )Ts = 2.50 meter (trim of the vessel)

Corrected dip:

 = 0.14 + ((2.00- 0.2088) x 0.0076) = 0.14 + (1.7912 x 0.0076) = 0.1536 m

Check is Lw less than Lt:

We now enter the ship's calibration tables at even keel at a dip of 0.1536 / 2 = 0.08 m. In a imaginairy calibration table the volume for 0.08 m even-keel is read, being 16,032 Ltr.The wedge volume can now be calculated as:

  Ls Lw = Da x -----          Ts

         V x Da x Ls VW  = -------------------               Lt x Ts

((Y - DF) x Ts)  (27.49x2.50) 2.50 Da = D + -------------------------- = 0.14 + (( 2.00 - ----------------- ) x ------------ ) Ls 329.20 329.20

Ls  0.1536 x 329.20 Lw = Da x ------ = -------------------------- = 20.23 m          Ts         2.50

V x Da x Ls  16,032 x 0.1536 x 329.20Vw = --------------------- = ------------------------------------------  = 8,107 ltr.      Lt x Ts           40.00 x 2.50

Page 151: Cargo Mate

IV.1.3. Wedge formula This SAYBOLT wedge-formula is only to be used with liquid, when the liquid doesn't touch all four bulkheads.By means of soundings the innage of the liquid is determined. On this innage a correction, (different from the trim correction from the calibration tables) has to be applied. This correction is calculated using the wedge formula.

Abbreviations used:Ls =length between perpendiculars Ts = trim of the vesselY = distance from the ullage point to the aft bulkheadDa = dip corrected to aft bulkheadD = observed dipDt = total height of the tank

First the measured dip has to be corrected as it if was measured at the aft bulkhead:

Next the length of the wedge is calculated by:

If Lw is less then the length of that particular cargo tank, the wedge formula is applicable.If the wedge formula is applicable, we now enter the ship's calibration tables for that particular tank, with the following dip value:

The wedge volume can now be calculated with the following formula:

in which: V =Volume found in ships calibration tables at even keel at dip Da/2.

Example:Measured dip D = 14 cm = 0.14 meter Y = 2.00 meter ( distance from the ullage point to the aft bulkhead )Dt = 27.49 meter ( total height of the tank ) Lt = 40.00 meter ( length of the tank )Ls = 329.20 meter (length between perpendiculars )Ts = 2.50 meter (trim of the vessel)

Corrected dip:

 = 0.14 + ((2.00- 0.2088) x 0.0076) = 0.14 + (1.7912 x 0.0076) = 0.1536 m

Check is Lw less than Lt:

We now enter the ship's calibration tables at even keel at a dip of 0.1536 / 2 = 0.08 m. In a imaginairy calibration table the volume for 0.08 m even-keel is read, being 16,032 Ltr.The wedge volume can now be calculated as:

Page 152: Cargo Mate

IV.1.3. Wedge formula This SAYBOLT wedge-formula is only to be used with liquid, when the liquid doesn't touch all four bulkheads.By means of soundings the innage of the liquid is determined. On this innage a correction, (different from the trim correction from the calibration tables) has to be applied. This correction is calculated using the wedge formula.

Abbreviations used:Ls =length between perpendiculars Ts = trim of the vesselY = distance from the ullage point to the aft bulkheadDa = dip corrected to aft bulkheadD = observed dipDt = total height of the tank

First the measured dip has to be corrected as it if was measured at the aft bulkhead:

Next the length of the wedge is calculated by:

If Lw is less then the length of that particular cargo tank, the wedge formula is applicable.If the wedge formula is applicable, we now enter the ship's calibration tables for that particular tank, with the following dip value:

The wedge volume can now be calculated with the following formula:

in which: V =Volume found in ships calibration tables at even keel at dip Da/2.

Example:Measured dip D = 14 cm = 0.14 meter Y = 2.00 meter ( distance from the ullage point to the aft bulkhead )Dt = 27.49 meter ( total height of the tank ) Lt = 40.00 meter ( length of the tank )Ls = 329.20 meter (length between perpendiculars )Ts = 2.50 meter (trim of the vessel)

Corrected dip:

 = 0.14 + ((2.00- 0.2088) x 0.0076) = 0.14 + (1.7912 x 0.0076) = 0.1536 m

Check is Lw less than Lt:

We now enter the ship's calibration tables at even keel at a dip of 0.1536 / 2 = 0.08 m. In a imaginairy calibration table the volume for 0.08 m even-keel is read, being 16,032 Ltr.The wedge volume can now be calculated as:

Go To Menu Go To Menu

Page 153: Cargo Mate

IV.1.3. Wedge formula This SAYBOLT wedge-formula is only to be used with liquid, when the liquid doesn't touch all four bulkheads.By means of soundings the innage of the liquid is determined. On this innage a correction, (different from the trim correction from the calibration tables) has to be applied. This correction is calculated using the wedge formula.

Abbreviations used:Ls =length between perpendiculars Ts = trim of the vesselY = distance from the ullage point to the aft bulkheadDa = dip corrected to aft bulkheadD = observed dipDt = total height of the tank

First the measured dip has to be corrected as it if was measured at the aft bulkhead:

Next the length of the wedge is calculated by:

If Lw is less then the length of that particular cargo tank, the wedge formula is applicable.If the wedge formula is applicable, we now enter the ship's calibration tables for that particular tank, with the following dip value:

The wedge volume can now be calculated with the following formula:

in which: V =Volume found in ships calibration tables at even keel at dip Da/2.

Example:Measured dip D = 14 cm = 0.14 meter Y = 2.00 meter ( distance from the ullage point to the aft bulkhead )Dt = 27.49 meter ( total height of the tank ) Lt = 40.00 meter ( length of the tank )Ls = 329.20 meter (length between perpendiculars )Ts = 2.50 meter (trim of the vessel)

Corrected dip:

 = 0.14 + ((2.00- 0.2088) x 0.0076) = 0.14 + (1.7912 x 0.0076) = 0.1536 m

Check is Lw less than Lt:

We now enter the ship's calibration tables at even keel at a dip of 0.1536 / 2 = 0.08 m. In a imaginairy calibration table the volume for 0.08 m even-keel is read, being 16,032 Ltr.The wedge volume can now be calculated as:

Page 154: Cargo Mate

IV.1.3. Wedge formula This SAYBOLT wedge-formula is only to be used with liquid, when the liquid doesn't touch all four bulkheads.By means of soundings the innage of the liquid is determined. On this innage a correction, (different from the trim correction from the calibration tables) has to be applied. This correction is calculated using the wedge formula.

Abbreviations used:Ls =length between perpendiculars Ts = trim of the vesselY = distance from the ullage point to the aft bulkheadDa = dip corrected to aft bulkheadD = observed dipDt = total height of the tank

First the measured dip has to be corrected as it if was measured at the aft bulkhead:

Next the length of the wedge is calculated by:

If Lw is less then the length of that particular cargo tank, the wedge formula is applicable.If the wedge formula is applicable, we now enter the ship's calibration tables for that particular tank, with the following dip value:

The wedge volume can now be calculated with the following formula:

in which: V =Volume found in ships calibration tables at even keel at dip Da/2.

Example:Measured dip D = 14 cm = 0.14 meter Y = 2.00 meter ( distance from the ullage point to the aft bulkhead )Dt = 27.49 meter ( total height of the tank ) Lt = 40.00 meter ( length of the tank )Ls = 329.20 meter (length between perpendiculars )Ts = 2.50 meter (trim of the vessel)

Corrected dip:

 = 0.14 + ((2.00- 0.2088) x 0.0076) = 0.14 + (1.7912 x 0.0076) = 0.1536 m

Check is Lw less than Lt:

We now enter the ship's calibration tables at even keel at a dip of 0.1536 / 2 = 0.08 m. In a imaginairy calibration table the volume for 0.08 m even-keel is read, being 16,032 Ltr.The wedge volume can now be calculated as:

Page 155: Cargo Mate

WEDGE Calculations (ROB / OBQ)

Y

D1

H

a

a

V=L×B×D2

2T

D= [D1×cosecα+(Y−H×tanα ) ]×tanα

Page 156: Cargo Mate

tanα=TL

Page 157: Cargo Mate

WEDGE Calculations (ROB / OBQ)

Использование этой формулы предполагает, что:Крен отсутствуетВсе величины выражены в метрахДнище танка не полностью покрыто грузомВсе остатки груза стекли в кормовую часть танка

где

V -объём остатков грузаL -длина судна между перпендикулярамиB -ширина танка

D -откорректированный взлив груза в танкеT - дифферент судна

Наибольшую проблему представляет собой расчет откорректированного взлива груза в танке, который производится следующим образом:

D1- измеренный взлив остатков груза в танкеY - отстояние мерительной точки от кормовой переборки танкаa - угол дифферентаH - высота танка.

Y

D1

H

a

a

V=L×B×D2

2T

D= [D1×cosecα+(Y−H×tanα ) ]×tanα

Page 158: Cargo Mate

Для определения угла дифферента α следует использовать свойство прямоугольного треугольника: «тангенс острого угла прямоугольного треугольника равен отношению противолежащего катета к прилежащему», то есть:

тангенс угла дифферента будет равен отношению дифферента судна Т длине судна между перпендикулярами.

tanα=TL

Page 159: Cargo Mate

WEDGE Calculations (ROB / OBQ) Go To Menu Go To Menu

Page 160: Cargo Mate

WEDGE Calculations (ROB / OBQ)

FWD 9.00 Tank I Ic Y RH L W A VAFT 12.00 No. (m) (m) (m) (m) (m) (m) (m) (Cub.m)

Trim 3.00 1C 0.01 0.37 12.24 29.360 51.2 21.82 0.12 17.3692

L.B.P. 320.00 2C 0.01 0.42 6.62 29.360 51.2 21.82 0.07 5.6182

3C 0.01 0.42 6.62 29.360 51.2 21.82 0.07 5.6182

V = ( W x A x A ) / ( 2 x f ) 4C 0.01 0.42 6.62 29.360 51.2 21.82 0.07 5.6182

5C 0.01 0.39 7.62 29.370 49.5 21.82 0.08 7.2364

Ic = ( L - Y ) x f 1P 0.01 0.42 6.32 29.180 51.2 9.98 0.07 2.3670

Aa = I + ( Y x f ) abridged or 1S 0.01 0.42 6.32 29.180 51.2 9.98 0.07 2.3670

A = I+( Y x f ) - ( RH x f x f ) unabridged 2P 0.01 0.42 6.92 29.140 51.2 9.98 0.07 2.7834

f = 0.009375 (Trim / LBP) 2S 0.01 0.42 6.92 29.140 51.2 9.98 0.07 2.7834

3P 0.01 0.42 6.42 29.080 51.2 9.98 0.07 2.4346

I - Innage ( dipping) 3S 0.01 0.42 6.42 29.080 51.2 9.98 0.07 2.4346

Ic - Critical innage ( Wedge formula is applicable if I < Ic only ) 4P 0.01 0.42 6.12 29.090 51.2 9.98 0.06 2.2363

A - Height of wedge at bulkhead 4S 0.01 0.42 6.12 29.090 51.2 9.98 0.06 2.2363

L - Length of tank 5P 0.01 0.25 8.74 29.090 35.84 0.09 0.0000

RH - Reference height of tank (table) 5S 0.01 0.25 8.74 29.090 35.84 0.09 0.0000

W - Width of tank (bottom) Slop P 0.03 11.84 29.300 15.36

Y - Distance between gauge point and aft bulkhead Slop S 0.03 11.84 29.300 15.36

TOTAL 61.1027

Y

L WW

RH

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Page 161: Cargo Mate

WEDGE Calculations (ROB / OBQ)

Tank d D Wedge V A B Y W L R

No. (m) (m) (Y or N/A) (Cub.m) (m) (m) (m) (m) (m) (m)

FWD 9.00 1 C 0.01 0.12 Y 17.2 29.541 29.860 12.24 21.82 51.20 29.36 AFT 12.00 2 C 0.01 0.07 Y 5.6 29.544 29.854 6.62 21.82 51.20 29.36 Trim 3.00 3 C 0.01 0.07 Y 5.6 29.543 29.858 6.62 21.82 51.20 29.36

L.B.P. 320.00 4 C 0.01 0.07 Y 5.6 29.545 29.878 6.62 21.82 51.20 29.36

Q 0.009375 5 C 0.01 0.08 Y 7.2 29.553 29.868 7.62 21.82 49.50 29.37 f 0.993 1 W 0.01 0.07 Y 2.4 29.367 29.662 6.32 9.98 51.20 29.18

2 W 0.01 0.07 Y 2.8 29.323 29.643 6.92 9.98 51.20 29.14 V = (D² x LBP x W) ÷ 2T 3 W 0.01 0.07 Y 2.4 29.262 29.580 6.42 9.98 51.20 29.08

4 W 0.01 0.06 Y 2.2 29.298 29.591 6.12 9.98 51.20 29.09 Factor = Q(Y - RQ). 5 W 0.08 Y - 29.373 29.680 8.74 - 35.84 29.09 Wedge only exists if L > (D ÷ Q) Slop's 0.11 Y - 29.485 29.783 11.84 - 15.36 29.30

D = d + Factor. = d + Q(Y - RQ).

LBP = Length between perpendiculars (in metres). A = Height from vapour control valve to tank bottom - zero sounding.d = Observed dip (in metres). B = Height from zero ullage point to tank bottom - zero sounding. D = Dip at the after bulkhead (in metres). Y = Distance of after bulkhead from dipping point. T = Trim (in metres). W = Width of tank at zero sounding datum - tank bottom. Q = Trim factor, (Trim ÷ LBP) (in metres). L = Length of tank. f = factor supplied by shipyard R = Reference height, (height of swinging point).

NOTES for VLCC "CHELSEA"The tank bottoms of all of the centre tanks are box formed and will give an exact wedge. It should be noted however that 1 C is only box formed over the last 36m of the compartment. The tank bottoms of 2W, 3W, and 4W are box formed, but the outer bulkheads are inclined, (into the ballast tanks), and therefore the wedge will not be strictly accurate.1 W, 5W, and the slop tanks are not square formed and data on the following pages have been taken directly from the calibration tables.

Length and breadth data has been derived from drawing "Midships Section DA200H001" (Box SA 1 /2), which gives a frame spacing of 5.12m between frames 51-111 and 3.42m for frames 50-51 for 5C. Reference heights and swinging points are taken from data in the Vapour Control Valve calibration tables.

Data tabulated on the following pages shows calculated wedge volumes. Note that 1 W, 5W, and the Slop tanks are not wedged, and data has been taken directly from the calibration tables. All wedged volumes have been adjusted by a factor of 0.993 to allow for permeability. This factor which was supplied by the shipyard has been applied to data in the Trim and Stability Book and to all volumes in the Calibration tables.

NOTES for VLCC "CHELSEA"The tank bottoms of all of the centre tanks are box formed and will give an exact wedge. It should be noted however that 1 C is only box formed over the last 36m of the compartment. The tank bottoms of 2W, 3W, and 4W are box formed, but the outer bulkheads are inclined, (into the ballast tanks), and therefore the wedge will not be strictly accurate.1 W, 5W, and the slop tanks are not square formed and data on the following pages have been taken directly from the calibration tables.

Length and breadth data has been derived from drawing "Midships Section DA200H001" (Box SA 1 /2), which gives a frame spacing of 5.12m between frames 51-111 and 3.42m for frames 50-51 for 5C. Reference heights and swinging points are taken from data in the Vapour Control Valve calibration tables.

Data tabulated on the following pages shows calculated wedge volumes. Note that 1 W, 5W, and the Slop tanks are not wedged, and data has been taken directly from the calibration tables. All wedged volumes have been adjusted by a factor of 0.993 to allow for permeability. This factor which was supplied by the shipyard has been applied to data in the Trim and Stability Book and to all volumes in the Calibration tables.

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Page 162: Cargo Mate

NOTES for VLCC "CHELSEA"The tank bottoms of all of the centre tanks are box formed and will give an exact wedge. It should be noted however that 1 C is only box formed over the last 36m of the compartment. The tank bottoms of 2W, 3W, and 4W are box formed, but the outer bulkheads are inclined, (into the ballast tanks), and therefore the wedge will not be strictly accurate.1 W, 5W, and the slop tanks are not square formed and data on the following pages have been taken directly from the calibration tables.

Length and breadth data has been derived from drawing "Midships Section DA200H001" (Box SA 1 /2), which gives a frame spacing of 5.12m between frames 51-111 and 3.42m for frames 50-51 for 5C. Reference heights and swinging points are taken from data in the Vapour Control Valve calibration tables.

Data tabulated on the following pages shows calculated wedge volumes. Note that 1 W, 5W, and the Slop tanks are not wedged, and data has been taken directly from the calibration tables. All wedged volumes have been adjusted by a factor of 0.993 to allow for permeability. This factor which was supplied by the shipyard has been applied to data in the Trim and Stability Book and to all volumes in the Calibration tables.

NOTES for VLCC "CHELSEA"The tank bottoms of all of the centre tanks are box formed and will give an exact wedge. It should be noted however that 1 C is only box formed over the last 36m of the compartment. The tank bottoms of 2W, 3W, and 4W are box formed, but the outer bulkheads are inclined, (into the ballast tanks), and therefore the wedge will not be strictly accurate.1 W, 5W, and the slop tanks are not square formed and data on the following pages have been taken directly from the calibration tables.

Length and breadth data has been derived from drawing "Midships Section DA200H001" (Box SA 1 /2), which gives a frame spacing of 5.12m between frames 51-111 and 3.42m for frames 50-51 for 5C. Reference heights and swinging points are taken from data in the Vapour Control Valve calibration tables.

Data tabulated on the following pages shows calculated wedge volumes. Note that 1 W, 5W, and the Slop tanks are not wedged, and data has been taken directly from the calibration tables. All wedged volumes have been adjusted by a factor of 0.993 to allow for permeability. This factor which was supplied by the shipyard has been applied to data in the Trim and Stability Book and to all volumes in the Calibration tables.

Page 163: Cargo Mate

D - Gauge heightS - Sounding (innage)U - Distance from sounding point to aft bulkheadW - Width of tank

LBP : 320.00 Mtrs L - Length of tankDraft FWD : 15.00 Mtrs LBP - Length between perpendiculars

Draft Aft : 20.00 Mtrs F - Trim factor ( Trim / LBP)Trim : 5.00 Mtrs A - Adjusted innage at aft bulkhead of tank [ ( U - D * F ) * F ] + S

Trim Factor : 0.015625 Note

CARGO TANKS DATA OBQ/ROB OIL OBQ/ROB WATER

Tank U D W L S A L*F Wedge Volume S A L*F

No. Mtrs Mtrs Mtrs Mtrs Mtrs (U-D*F)*F+S Y / N Cub.m. Mtrs (U-D*F)*F+S

1C 12.24 29.360 21.820 51.20 0.01 0.1940820 0.8000000 Y 26.30 0.01 0.1940820 0.80000002C 6.62 29.360 21.820 51.20 0.01 0.1062695 0.8000000 Y 7.89 0.01 0.1062695 0.80000003C 6.62 29.360 21.820 51.20 0.01 0.1062695 0.8000000 Y 7.89 0.01 0.1062695 0.80000004C 6.62 29.360 21.820 51.20 0.01 0.1062695 0.8000000 Y 7.89 0.01 0.1062695 0.80000005C 7.62 29.370 21.820 49.50 0.01 0.1218921 0.7734375 Y 10.37 0.01 0.1218921 0.77343751P 6.32 29.180 9.980 51.20 0.01 0.1016260 0.8000000 Y 3.30 0.01 0.1016260 0.80000001S 6.32 29.180 9.980 51.20 0.01 0.1016260 0.8000000 Y 3.30 0.01 0.1016260 0.80000002P 6.92 29.140 9.980 51.20 0.01 0.1110107 0.8000000 Y 3.94 0.01 0.1110107 0.80000002S 6.92 29.140 9.980 51.20 0.01 0.1110107 0.8000000 Y 3.94 0.01 0.1110107 0.80000003P 6.42 29.080 9.980 51.20 0.01 0.1032129 0.8000000 Y 3.40 0.01 0.1032129 0.80000003S 6.42 29.080 9.980 51.20 0.01 0.1032129 0.8000000 Y 3.40 0.01 0.1032129 0.80000004P 6.12 29.090 9.980 51.20 0.01 0.0985229 0.8000000 Y 3.10 0.01 0.0985229 0.80000004S 6.12 29.090 9.980 51.20 0.01 0.0985229 0.8000000 Y 3.10 0.01 0.0985229 0.80000005P No Wedhge Applied 0.0000000 0.0000000 Y 0 0.0000000 0.00000005S No Wedhge Applied 0.0000000 0.0000000 Y 0 0.0000000 0.0000000

SLP No Wedhge Applied 0.0000000 0.0000000 Y 0 0.0000000 0.0000000SLS No Wedhge Applied 0.0000000 0.0000000 Y 0 0.0000000 0.0000000

: If (A) > (L*F) then do not apply Wedge Formula

{ [ ( U - D * F ) * F ] + S } ^ 2 x WWedge Formula = -------------------------------------------------

2 F

{ [ ( U - D * F ) * F ] + S } ^ 2 x WWedge Formula = -------------------------------------------------

2 F

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Page 164: Cargo Mate

OBQ/ROB WATER FREE WATER IN CARGO

Wedge Volume S A L*F Wedge Volume

Y / N Cub.m. Mtrs (U-D*F)*F+S Y / N Cub.m.

Y 26.30 0.01 0.1940820 0.8000000 Y 26.30Y 7.89 0.01 0.1062695 0.8000000 Y 7.89Y 7.89 0.01 0.1062695 0.8000000 Y 7.89Y 7.89 0.01 0.1062695 0.8000000 Y 7.89Y 10.37 0.01 0.1218921 0.7734375 Y 10.37Y 3.30 0.01 0.1016260 0.8000000 Y 3.30Y 3.30 0.01 0.1016260 0.8000000 Y 3.30Y 3.94 0.01 0.1110107 0.8000000 Y 3.94Y 3.94 0.01 0.1110107 0.8000000 Y 3.94Y 3.40 0.01 0.1032129 0.8000000 Y 3.40Y 3.40 0.01 0.1032129 0.8000000 Y 3.40Y 3.10 0.01 0.0985229 0.8000000 Y 3.10Y 3.10 0.01 0.0985229 0.8000000 Y 3.10Y 0.00 0.0000000 0.0000000 Y 0.00Y 0.00 0.0000000 0.0000000 Y 0.00Y 0.00 0.0000000 0.0000000 Y 0.00Y 0.00 0.0000000 0.0000000 Y 0.00

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Page 165: Cargo Mate

ASTM 6 A - Tafel or Routine, Tab. 56

A, B of D A 0.99895 1.00105

Tafel of Routine r 0.9758

API 60°F 31.00

Temp°F 100.00 6.292 Tab.52

VCF 0.9819

API 31

D 869.91 Bbls to m³ 25

T 40 Tab.# 4

alpha A 0.0004507

VCF 0.9819

alpha 1 0.0005346

alpha 2 0.0000993

alpha 3 0.0004365

alpha 4 0.0004478

alpha B 0.0004478

VCF 0.9820

alpha D 0.0004009

VCF 0.9839

rounding format

100.00 temp

31.00 API

31.00 API

100.00 temp

ASTM 54 A

A, B of D A

Tafel of Routine R

Dens 0.8330

Temp 35.00

VCF 0.9822 D 833T 20alfa54A 0.0008848 VCF 54A 0.9822 alfa541 0.0010260 alfa542 0.0004996 alfa543 0.0008568 alfa544 0.0008531 alfa54B 0.0008568

Page 166: Cargo Mate

VCF 54B 0.9828 alpha 0.0007537 VCF 0.9849

rounding format35.0 temp fr tab

0.8330 density fr tab833.0

0.8340140.0

35.0

MtBbl(API) MtBbl = 1.01605 * (22.12362536 / (API + 131.502609) - 0.0001927941766)

LtBbl(API) LtBbl = 0.98421 * (1.01605 * (22.12362536 / (API + 131.502609) - 0.0001927941766))

APISG(SG) APISG = (141.5 / SG) - 131.5

SGAPI(API) SGAPI = 141.5 / (API + 131.5)

Table 11 TAB11 = (589.943 / (API + 131.5) - 0.0050789) * 0.037530 0.13679

#NAME?Table 13

30 0.13899 TAB13 = (535.1911 / (API + 131.5) - 0.0046189) * 0.042#NAME?

Table 830 7.296

#NAME?#NAME?

Table 56 from Air to Vac Tab56AV(Wdens As Single)Tab56AV = (myInt((Wdens / (1.0001506 * Wdens - 0.0012202)) * 10000) + 0.5) / 10000

1.07 1.00095

Table 56 from Vac to Air Tab56VA(Wdens As Single)Tab56VA = ((myInt((1.0001506 - (0.0012202 / Wdens)) * 10000) + 0.5)) / 10000

CONVERTS DENCITY AT 15C IN VACUUM TO CORRESPONDING DENCITY AT 15C IN AIRDENC_AIR = ((DENC_VAC) * 1.0001506) - 0.0012202

0.9653 0.9642

Page 167: Cargo Mate

Table 11 Table 13 Table 29t (1,2 of 1 2 3 11API 60 39.21000 39.00000 0.75400 13

0.12940 0.13164 0.11769 29A 1 1 1F 2,240.00 2,204.62 2,204.62 A1 39.20 39 0.7

0.15892 W 0.01 0 0.0540.15892 A2 39.3 0 0.8

D1 0.82893966 0.82991202 1.07034796 B1 0.12940984 0.13164109 0.16983537 X 0.00000000 0.00000000 0.00000000 E_1 0.12940944 0.13164069 0.16983487 E_2 0.12940930 0.13164060 0.16983470 E1 0.12940944 0.13164060 0.00000000 D1! 0.12941000 0.13164000 0.00000000 D2 0.82845433 1.07604563 1.06953893 B2 0.12933396 0.17074047 0.16970685 X 0.00000000 0.00000000 0.00000000 E_1 0.1293334636 0.1707399692 0.1697063519E_2 0.12933330 0.17073980 0.16970620 E2 0.12933346 0.17073980 0.00000000 D2! 0.12933000 0.17074000 0.00000000 C 0.12940000 0.13164000 0.00000000 A1 39.21 39 0.754W 0 0 0A2 0 0 0B1 6.13010601 6.09727351 0.11769338 E1 6.1301056058 6.097273105 0.1176932829D1 6.13011000 6.09727000 0.11769000 B2 (0.00019093) (0.00019093) (0.00019093)E2 (0.00019133) (0.00019133) (0.00019103)D2 (0.00018000) (0.00018000) (0.00018000)C_3 6.13011000 6.09727000 0.11769000

Page 168: Cargo Mate

MtBbl = 1.01605 * (22.12362536 / (API + 131.502609) - 0.0001927941766)

LtBbl = 0.98421 * (1.01605 * (22.12362536 / (API + 131.502609) - 0.0001927941766))

Page 169: Cargo Mate

Table 29 Ltons/Bbl-60°F t (1,2 of 3) 3 Mtons/Bbl-60°F R.DENS (60/60) 0.87640 Ltons/Bbl 60°F 0.14302 T. 29 - For Relative Density 60/60°F A1 0.876

W 0.0004A2 0.976B1 0.13676750 E1 0.1367672025D1 0.13677000 B2 0.15240203 E2 0.15240193 D2 0.15240000 C_3 0.14302000

Page 170: Cargo Mate

Table 29R.DENS (60/60) 0.91950 A1 0.91950 B1 0.14356852 E1 0.1435682205D1 0.14357

Page 171: Cargo Mate

Copyright © 2001 - 2007 Version: 27 May 2007 This program is written by Capt. Yury Shishkin This program is collection of small programs or formulas for Cargo Calculations.

1. All Pages in this File is separate. 2. You Can Cut or Copy any Page from this File and Put in to Yours Programs.

Please contact [email protected] if you have any formulas or suggestions to improve this program.

No liability can be claimed for errors resulting from the use of this program.

Copyright © 2001 - 2007 Version: 27 May 2007 This program is written by Capt. Yury Shishkin This program is collection of small programs or formulas for Cargo Calculations.

1. All Pages in this File is separate. 2. You Can Cut or Copy any Page from this File and Put in to Yours Programs.

Please contact [email protected] if you have any formulas or suggestions to improve this program.

No liability can be claimed for errors resulting from the use of this program.

Notes:

Page 172: Cargo Mate

Copyright © 2001 - 2007 Version: 27 May 2007 This program is written by Capt. Yury Shishkin This program is collection of small programs or formulas for Cargo Calculations.

1. All Pages in this File is separate. 2. You Can Cut or Copy any Page from this File and Put in to Yours Programs.

Please contact [email protected] if you have any formulas or suggestions to improve this program.

No liability can be claimed for errors resulting from the use of this program.

Copyright © 2001 - 2007 Version: 27 May 2007 This program is written by Capt. Yury Shishkin This program is collection of small programs or formulas for Cargo Calculations.

1. All Pages in this File is separate. 2. You Can Cut or Copy any Page from this File and Put in to Yours Programs.

Please contact [email protected] if you have any formulas or suggestions to improve this program.

No liability can be claimed for errors resulting from the use of this program.

Notes: