F-15C_Eagle_SAC_-_February_1992

8/7/2019 F-15C_Eagle_SAC_-_February_1992

1/10

SERVICE

STANDARD A IRCRAFT CHARACTER ISTICSBY AUTHORITY OFTHE SECRETARYOF THE AIR FORCE

F-ISCEAGLE

MCDONNELL DOUGLAS

TwoF-I00-PW-220Prall & Whitney

Feb 92 (AFG 2. voi-r. Addn 61) (69 of 228) F-ISC (220 engine) O S 9 - :


2/10

SERVICE

Wing Area 608 sq raAspect Rat io 3.01M.A.C. . ... . .. . 191.28 In

Wing Sec l ionRoot ........... NACA 64A006.6Tip ............ NACA 64A20J.0

4l1 l i gal.,"t.at Tn

'100al.e.ternalTn

- 28.2511-

AIM-7 MI.. lles 6100al.e..ternal Tenk

F-ISC (220 engine)2

(70 of 228) (AFG 2. Vol-I. Addn 61) Feb 92


3/10

SERVICEPOWE~ PLANT MIS SION AND DESCR IP TION WEIGHTS LOAD

No. '" Model . .. (1) FlDO-PW-110 lOADINGS LIl fACW.lMfr Prall ' " Whi lney Navy Equivalenl: None Manufaclurer', Model: 199-IC Emp'Y ........... 28.476 (A) ... . 7.33............Engine Spec. No. CP1I344A The F-ISC is a single-place, land based, Iwin jet, high performance air B.lie ............. ".7Jl . ...... 6.00.... . Baa ie F li,h , Du il n . )7,400 . ...... 7.llType .... . Twin Spool. Turbofan superiorily fighler. The principle mission of Ihe F-I SC i s 10 assure decis ive Combl' ........... 41.286 ...... 6.64Lenglh ............... 208.13 In. supremacy In the air. The airplane has the addilional capabilily 10 p erform an IoIIIIT.O .......... 68.000t ...... 4.01a ll ac lt mis si on wi lh conventi onal ext er nal ly mount ed weapons and mis si le s. . .. .ndinl Dui ,n . .. . l S, OO O . . . .... 7.11Diameler (Nom) ........ 46.S in. Basic armamenl is an M61AI gun and four air-la-air Sparrow missiles. The 1 0 1 11 1 . .. . ndinl DuilnWeighl (dry) ............. 3200 Ib M61 A I gun is moun led in Ihe riahl hand wing roo I fillel, afl of Ihe engine inlet Wei,hl ......... 44.100 ....... 6.19NOZZle ........ CD Balanced Beam while the missiles are carried on the fuselage on corner mounted submergedAugmentation ......... Aflerburner raclts. A fuselage centerline store station plus Inner wing store stations are (A) AClual F-ISC IoISIP

p rovided fo r ca rr iage o f e it her 610 gallon I uel tanks o r au-t o- ground weaponry. for Million It loIaximum Spee Limll Wei,hlThe a ir pl ane is capab le o f be ing re fuel ed i n-f lighl. . . 10.0 fII.ec DCli,n Rile 01 SinkENGINE RATINGS Special [eatures of Ihe F-ISC are swepl wings and tails, Iwin vertical tails. FUELa ll -moving d if fe renl ia ll y con tro lled hori zonta l ta il s, au toma ti ca ll y coni r olled

SL Sialic Ib RPM (NI/N2) exte rnal compres si on engi ne a ir i nle ts wil h t hr ee overhead ramps, and I ra il ing IO'6IIOti tiO 16ti~ !iALedge flaps for low speed operations. Lateral control is achieved by Ihe FUI, inl ............ )........ " 1078-Max: 23,4S0 10,010/12,960 d if fe renli al ly con tro lled horizont al la lls in combina ti on with t he a il er ons . Win, . Inr ........... 1 . .......... 992Mil: 14,370 10,010/12,960 Fu. EXI. Drop ....... I ........... 610Win, ., Ex" Drop .. ... 1 . ... .. ... . illll'Max COni 11,420 9790/12,440 The avionics subsystems provide Ihe capabilily for communicauons , To,"1 )900navi ga tion, iden ti fi ca li on, dete ct ion t hr ea t wa rni ng . a rmament con tr ol, a tt ack

s te er ing, and compu tauonal funct ions requ ired dur ing mis sion opera ti ons. The Tlnk No. I .... Blldder; Tlnk. No.1 IndMill Fire Coni rol led Systems (FCS) provides an etlecuve weapons systems capabil ily No. ) . .. Sell-Sellin,, fo r v isual and a ll -weather a ir -to -ai r and ai r- Io -g round mis si ons. P rovis ions f or Grade .................... 1P-4 or JP-S30 a Tactica] Electronics Warfare System (TEWS) are provided. Speeili elli on .. ... .. ... ... .. "IL- T-5624Coni OILEquipmem includes a pressurized cockpil wilh an ACES II ejection seal, En,lne ........ 5 , lllen, ..... 10 (Total)Uninsta lled, Per Ensine liquid oxyaen sysl em, and snu-G non-p re ssu re sui I pr ovi si ons. Spcei ll el lion . .. .. . MIL-L-710a Ind MIL- Wilh allerburner operaling Development L-11699

Contract ............................................... Feb 1983 ELECfRONICSDIMENSIONS Firsl Flight 0 0.0 0 0.0 Jun 1985First Squadron Delivery ................................... Jun 1985WingSpan ................. 42.81 flSweepbacl t (LE) 00 0 0 0 4S - BOMBS GUNSIncidence .................. ODihedral .................. -l- One gun mounted in right hand See Page 10.wing root Iillet afl of Ihe engine in-

See STORE LOADINGS, Page 9. lei.Length ................. 63.7S IIHeighl ................ 18.S8 II Type Size RdsTread .................. 9.03 n M61AI 20 mmWheelbase 17.78 II .. . ...... 9400 000 0.

Feb 92 (AFG 2. Vol-I. Addn 61) (71 of 228) F-15C (220 engine)3


4/10


5/10

Take-Off12

10

8Oislanall 6I,OOOn

4

2

- ..L_!., s.1l_-"-r_ClNfl iO., \

~ /G"_Run~ '/\~r-,

~ v ~ ~- - l . . - . : : : : = o ' ~ --. . . - .__- -~-64

1,600

ClimbSERVICE

o28 36 52 56 60

Al l i lUde

1.3

32G rO S& W e ig hl - 1,000 Ib

031._11",A"'-lf~~+---~~~---+--~--~ 043.13111'"A ...lfP ...(2).. K14

Speed60

20

o ~ ~ ~ - - - ~ - - - - ~ - - - - ~ - - ~ - - - - _ . - - - - - - - - ~o 600 1,200 1,400800Knots 1,000200 400Feb 92 (AFG 2. Vol-t. Addn 6t) (73 of 228)

~~~~----~~~~--~----+----;----~----1t .o o o n

Aale 01Cl imb - 1,000 " 'm in

Maneuverability12

10

8loadFactor 6

g4

2

r - D - J W ~ o n gL o r n J S I C_GW.3IUI4611lO.OOOft_lOOdF .......... .,'., .. ., ......... J ...... ... - -- !r - -rz . ., . . . .~ t--- ............u..bIe

~ V ~.s .. _~ ~~ ' - - - . I u_p_~ ~~~,.. . ~ ~ .. . . s...._- ~ - : r


6/10

SERVICE

Specific E xc ess Power

Ahi tudet . o oo n

Maximum Power70 C-.

GW.:!6._1b

Mach Numbef

Maximum Power70 c-.

GW. J I I . !N81b60 n. 50g

50

Ahi tude 40i .o o o e 30

20

10

0 0

Military Powerror---~----.-----r---~----'-----r----'c_

1.4

GW. J I I . !N81b60 n.l0g

Mach Number

F-15C (220 engine)6

50

Altitude 40t .o o o n 30

20

10

028 0

1.2

1.6 2.0 2.4Mach Numbef

2.8 3.2

Military Powerro c_

GW. J I I .1M81b60 n.5.0g

A hi1 Ud e 4 0 1----+----+----1---+----+---11---+----1

o~--~---.~~-'~~~~L-~ __~ __~o 0.2 0.4 0.6 0.8Mach Numbef

1.2 1.41.0

(74 of 228) (AFG 2. voi-r. Addn 61) Feb 92

1.6


7/10

SERVICE

NOTESFormula: Radlul Million I (Air Superiority)

IA. Takcoff and Ac:celera tion Fuel Allowlncc (Sea Level, Siandard Day)1. Ground Ope ra lion - 6 min a t Thrus t 10 Weiaht Ra lio T/W . .0 .11 . Acce le ra te to Mach 0.3 a t Maximum Thrus l - No Dls tance Credi t

t1 Fuel .. mV (Wo - WI>1 (T -D)

3. Acce le ra le From Mach 0 .3 10 Inilial Climb Spccd al MililaryThrus t - No Distance Crcdi led

B. Military Thrust Climb From Sca Level 10 Optimum Cruise AunudeC. Cru isc Oul a l Spced aor' Al ti tude for Optimum Rangc (Cl imb t

Cruise . . 100 NM)D. Descend 10 10,000 ft - No Crcdil for Fuel or DistanceE. Dash to Target Arca at 10,000 fl a l Mach 0.85F. Combat Fuel Allowance: Equals Fuel Rcquircd 10 Allain 144,000 I tof

Maneuvcr EnerlY at 10,000 ft a l Mach 0.9 Usina Maximum ThrustIt1 Fuel .. 144,000 x , z I P .

(Calculaled Usina a Clean Aircraf t Wilh 50% Total Internal Fuel, p.a l 1.0 g Fl iahl , Retain Missi le s and Ammo Alte r Comba t)

G. Dash Back al 10,000 fl a l Mach 0.8SH. Mililary Thrust Climb From 10,000 fl 10 Oplimum Cruise AltitudeI. Cruise Back al Speed and Anuude for Optimum Range (Climb t

Cruise " 200 NM)J. Descend 10 Sea Leve l - No c redi t for Fue l or DistanceK. Rese rve s: 20 min a l Speed for Maximum Endurance a t Sea Leve l.

Both Engines OperatingFormula: Radlul Mission II (Close Air Support)A. Takeoff and Acceleration Fuel Allowance (Sea Level. Standard Day)

1. Ground Ope ra tion - 6 min a l Thrust to Weigh t Rat io TIW = 0.2

Formula: Radius Mission II (Clole Air Support) (Continued)2. Accelerate 10 Mach 0.3 a l Maximum Thrus t - No Distance Credi t. .t1 Fue l = mV (Wo - Wd1 (T -D)3. Accelerate From Mach 0.3 to Initial Climb Speed at Military

Thrust - No Distance Credi tedB. Mili ta ry Thrus t Climb From Sea Leve l 10 S O O O flC. Cru ise Out 10 Station al Speed for Optimum Range at S O O O ft (Climb t

Cruise = 100NM)D. Loi te r for Speci fic T ime a t 5000 f t a l Speed for Maximum EnduranceE. Combat Fuel Allowance Equals Fuel Required to Allain 50,000 It of

Maneuver Energy at 5000 fl IIMach 0.9 Using Maximum Thrust

.t1 Fuel .. 50,000 x w/P.(Calculated Using a Clean Aircraf l wilh 50% Tota l In te rna l Fue l, P ,at 1.0 g Fhght]

F. Initiate Search for Target and Drop Stores (Pylons. Racks, andAmmoRetained)

G. Cruise Back;10 Base (100 NM) a t Speed for Opt imum Range a l 5000 ftH. Descend 10 Sea Leve l - No Credi t for Fue l or DistanceI. Reserves: 20min at Speed for Maximum Endurance at Sea Level, Both

Engines Operating, Plus 5% of Initial Fuel LoadFormula: Radius Mission 111 and IV (Counter Air)A. Takeoff and Acceleration Fuel Allowance (Sea Level. Standard Day)

1. Ground Operation - 6 min at Thrust to Weighl Ratio T/W = 0.22. Accelerate 10 Mach 0.3 a t Maximum Thrus t - No Distance Credi t.t1 Fue l = mV (Wo - Wa)

2 (T -D)(Continued on page 8)

Feb 92 (AFG 2, voi-r. Addn 61) (75 of 228) F-15C (220 engine)

7


8/10

SERVICE 503~ - - - - - - - - - - - - - - - - - - - - - - - -NOTES

Formula: Radius Million III and IV (Counter Air) (Continued)

3. Accelerate From Mach 0.3 to Initial Climb Speed at MilitaryThrus t - No Distance Credi ted

B. Military Thrust Climb From Sea Level to Optimum Cruise Alt itudeC. Crui se Out a t Speed and Al ti tude for Optimum RangeD. Descend to 10.000 ft - No Credit for Fuel or DistanceE. Combat Fue l Allowance : Equal ! Fue l Required to Attaln 60.000 ft of

Maneuver Energy at 10.000 I t a t Mach 0.7 Using Military Thrust

6. Fuel = 60.000 x : / P ,(Calculated U!lng a Clean Aircraft With SO% Total Inte rnal Fue l. P , a t1.0 g Flight)

F . Drop S tores (Re ta in Py lon! , Racks, and Ammo)G. Mil it ary Thrus t C limb From 10,000 It to Optimum Cruise Alt itudeH. Cruis e Back a t Speed and Alt itude for Opt imum RangeI. Descend to Sea Level - No Cred it f or Fuel or DistanceJ . Rese rves: 20min a t Speed for Maxlmum Endurance a tSea Level , Both

Englne! Operating Plus S% of Initial Fuel LoadFormula: Radius Mission V (Area Intercept)A. Range Free Allowance forGround Operation, Takeorr and Acceleration

to Climb Speed Includes Fuel for 2 min at Maximum Continuous Thrustat Sea Level Static

B. Military Thrust Climb From Sea Level to Optimum Cruise Alt itudeC . Cruis e Out a t Speed and Alt itude for Opt imum RangeD. C limb a t Maximum Thrus ! to Subsonic Combat Ce il ingE. Combat at 50,000 ft, Mach 0.9 for 5Min at Maxlmum Thrust (Retain

Missi les and Ammo After Combat)F . Descend to Opt imum Subsonic Crui se Alt itude - No Credit for Fue l or

Distance

Formula: Radius Minion V (Area Intercept) (Continued)

G. Cruis e Back a t Speed and Alt itude for Optimum RangeH. Descend to Sea Level - No Credit fo r Fuel or DistanceI. Reserves: 20min at Speed for Maximum Endurance at Sea Level , Both

Engines Operating, Plus S% of Initial Fuel Load (This Mission Includesa S% Increase In Fuel Consumption as a Service Tolerance)

Formula: Range Minion VI (Ferry)A. Range Free Allowance for Ground Operation, Takeoff, and Acceleration

to Climb Speed Includes Fuel for 5 min at Maximum Continuous Thrustat Sea Level Static

B. Mil ita ry Thrus t Cl imb From Sea Level to Opt imum Cruise Alt itudeC. Cruise Out at Speed and Altitude for Optimum Range Until Only Reserve

Fuel RemainsD. Descend to Sea Level - No Credit fo r Fuel or DistanceE. Rese rves : 20min a t Speed for Maximum Endurance a t Sea Level , Both

Engines Operating, Plus S% of Initial Fuel Load (This Mission Includesa S% Increase In Fuel Consumption as a Service Tolerance)

General Minion Notes:

1. JP-4 Fuel at 6.S Iblgal2 . Ammunit ion I ! Inc luded In an Gross Weight s3 . Maxlmum Continuous thrust I s Defined as 8S% of Military Thrust4 . Air Super iori ty, C lose Air Support , and Counter Ai r Miss ions a re F-JS

Request for Proposal (RFP) Missions While the Area Intercept and FerryRange Missions are MIL-C-SOI JA Type Missions

Data Reference : Contrac tor' s Data Dated June 1986Revision Basis : Inl tlal Issue

F-t5C (220 engine)

8

76 of 228) (AFG 2, ver- t . Addn 61) Feb 92


9/10

SERVICE

External Store Loading - Supplemental

~.~'-I _>\

.. ,/ \ /\

Stores 9 8 7 6 5 4 3 2 1Air-loAir MissilesAIM-7F/M I I I 1AIM-9J/P/LIM 2 2AIM-120 AMRAAM 2 1 I I I 2General Purpose

MK-82 LDGP 6 6 6MK-82 Snakeye 6 6 6MK-84 LDGP 1 I IGuided WeaponsGBU-IOA/B, C/B I I IDispensersCBU-S2B/B 4 4 4CBU-SB/B 4 4 4CBU-71/B 4 4 4MK-20 Rockeye 6 6 6

Miscellaneous Stores610 gal lon fue l Tank - I I ISUU-20B/A I I IMXU-64B/A Cargo I I IMounling HardwareSUU-S9B/A Pylon I ISUU-60BI A Pylon IBRU-26A/A I I IADU-407A Adapler (AIM-9) 2 2LAU-114/A Launcher (AIM-9) 2 2LAU-12BI A Launcher (AIM-9) 2 2

G)/Top View

Feb 92 (AFG 2, ver-t. Addn 61) (77 of 228) F- lSC (220 engine)9


10/10

SERVICE

ELECTRONICS (Continued from page 3)Comm-Nav-Identirtcation System

Integrated Comm/Navlldent PanelComm/Nav/ldent Antenna GroupKY-58 Control PanelAutomatic Direction Finder SetUHF Receiver/TransmitterIFF Interrogator Recelver/TransmltterIFF TransponderIFF Reply EvaluatorTACAN Receiver/TransmitterInstrument Landing System ReceiverSecure Speech ................ KY-58Inter roga tion Computer KIR-IA/TSECCryto Computer KIT-IA/TSECAnt i Jam Comm (Prov)JTIDS (Prov)

Flight InstrumentsAirspeed Mach IndicatorAltitude IndicatorVertical Speed IndicatorAngle-of-Attack Indicator

Penetrat~n Aid (TEWS) SystemCount~rmeasures DispenserRadar ~arning Receive r SetInternal Countermeasures SetTEWS! Pod ProvisionsElectronic Warfare Warning SetInterference Blanker UnitTactical Information System (Prov)I

Propulsion SubsystemAir Inlet Controller System

Navigation SystemMagnetic AZ. Detector SensorInertial Navigation SetAlt itude and Heading Reference SetAir Data ComputerAOA SensorTotal Temperature ProbeOverspeed Detection Set

Central ComputerControl f,nd Display System

Head p Display SetVertic I Situation Display Set

IHorlzdntal Situation Display SetAltitude Director IndleatorVideo Tape RecorderMultipurpose Color Display UnitData Transfer Module

flight ControlAuto Flight Control Set Fire Control SystemProgrammable Armament Control Set

APG-63/APG-70 Radar SetLead Computing Gyro Unit

F-ISC (220 engine) 8 of 228) (AFG 2. ver- i . Addn 61) Feb 9210

F-15C_Eagle_SAC_-_February_1992

Documents

Transcript of F-15C_Eagle_SAC_-_February_1992