A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A...

118
k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information Facility FFN0 672 Aug 65 https://ntrs.nasa.gov/search.jsp?R=19800010096 2019-12-29T07:11:32+00:00Z

Transcript of A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A...

Page 1: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

k-CR Toxic level hypergOlic 33 vapor detection sensor

development.

A Reproduced Copy OF

t

Reproduced for NASA

by the

NASA Scientific and Technical Information Facility

FFN0 672 Aug 65

https://ntrs.nasa.gov/search.jsp?R=19800010096 2019-12-29T07:11:32+00:00Z

Page 2: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

N('VEMBER 28, 1979 FL 2C27 1('7L L1BFARY

NBEBG B CA 93437-6021

LITO ---AVAI-L-A E L C ^1py

NASA CONTRACT REPORT CR454633

TOXIC LEVEL HYPERGOLIC VAPOR DETECTION SEN DOR DEVELOPMENT

JOSEPH R. STETTER, Y1NG-KIT LAU, RAYMOND B. CROMER

PREPARED BY: ENERGETICS SCIENCE DIVISION OF BECTON DICKINSON & Co.

NAZi 0-0402

r CZ

c U c :•

) m

(HAS CR-1546J)) TOXIC LEVEL HYL3ERGOLICN80-18366

VAPOS DETECTION SENDOR DEVELOPMEST F inal Report (Energetics Science, Inc., Elmsford,

. T.) 16 p UC A06/MF AOl CSCL 1B Unclas G3/35 47279

Page 3: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

STA$DARD TITLE PAGE

1. Repo" N.. 3. Govenberent Accession" - t Recipient . . Cstoi. .4 CR-154633 4. ThI. and Subtitle s Reci,

Toxic Level 1{ypergolic Vapor Detection _November 28, 1979 Sensor Development ö. Performing O.ç&.u.ø Cod.

,. Ail.(,) J. RStetter, Ylng-KWLatçfl. B. Czomer o. 14,. Tech Reps: P.M. Rogers and ?&Scott KSC TR 28-1 9. Psdo,i.nq OtgonIa.so., Nsa. .d Add,... 10. W.h (hilt No.

John F. Kennedy Space CenterN.. Kennedy Space Center, Florida 32899 NASIO-9492

- 13. ?.p. of Q.p. and Potted Covered 13. Spo,oiu Agency No... s.d Adé...

Final Report National Aeronautics and Space Administration I. Seiis.tlsq Agency Cod.

IS. Abss

The space shuttle program at Kennedy Space Center will involve the use and handling of large quantities of hypergolic propellants including hydrazine (H), mor.omethy1hydraze (MMH), and unsymmetrical dimethylhydrazino (UDMH). Hydrazine compounds (H, MMH, and UDMH) are highly toxic, and threshold limit values (TLV) have been established by OSHA at 1.0 ppm H, 0.2 ppm MMH and 0.5 ppm UDMH.

There are not toxic level hydrazine vapor monitors commercially available meeting KSC's requirement for a low cost, accurate, reliable and simple to operate and maintain instrument which can read in the parts-per-billion, range. The objectives of NAS 10-9492 are: 1) to develop clectrochemical sensor technology capable of PPB level hypergolic vapor sensing, and 2) to design, fabricate and deliver to KSC o;e portable instrument capable of meeting the design goals. A report of the completing of this contract is the subject of this final report.

16. kay Words

Hydrazine Vapor Toxic Sensor Hypergolic Vapor Detection

I?. Bbhoi.hi1 CcivoI Ia. Dl.,sb.s.

Announce In Star Unlimited

19. S.cw,t, CIo..f.(of thisreport) 20. Scv.liy CIe.sif40, this page) 21. N.. of Pages 22,

NONE NONE 103 SIC PSIà 052?I*I dam.

Page 4: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

.- .1574 15

't I

TOOC LEVEL 1YPERGOUC VAPOR DETECTION SEOR DEVELOPMENT

FINAL REPORT NOVEMBER 2 9 11

NASA CONTRACT NAS 10-9492

ENERGETICS SCIENCE DIVISION OF BECTON DICKINSON&CO.

85 EXECUTh'E BOULEVARD

ELUSEORD. NEW YORK 10523

Page 5: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

National Aeronautics and Space Administration

John F. Kennedy Space Canter NASA Kennedy Space Center. Florida 32899

ReplytoAtinof. DLDED.32

TO: Distribution

FROM: DL-DEED-32/Chief, Data Support Systems Section

SUBJECT: Toxic Level Hypergolic Vapor Detection Sensor • Development, Final Report, HAS 10-9492

The subject report is enclosed for your information. DL-DED-32, in a joint NASA/USAF effort, will be performing

- additional testing and evaluating the new instrument. Plans are to procure additional instruments for use in this effort.

Please contact Mr. Scott (305-867-3842), or the undersigned if you have any questions.

RoLYGOs 9'ryy 1/4 - 1110—

Enclosure: as

Page 6: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TITLE:

AUTHORS:

SUBMITTED TO:

TOXIC LEVEL HYPERGOLIC VAPOR DETECTION SENSOR DEVELOPMENT

JOSEPH R. STETTER, YING-KIT LAU, RAYMOND 13, CROMER

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION KENNEDY SPACE CENTER FLORIDA 32899

•1

kow

NASA TECHNICAL MANAGERS: PERRY H. ROGERS AND MARSHALL SCOTT

CONTRACT NO.: HAS 10-9492

SUBMITTED BY: ENERGETICS SCIENCE DIVISION OF BECTON DICKINSON AND COMPANY 85 EXECUTIVE BOULEVARD ELMSFORD NY 10523

FINAL REPORT

NOVEMBER 28,. 1979

tw

Page 7: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

ACKNOWLEDGEMENTS

This report was prepared for the National Aeronautics and Space Administra-

tion, Kennedy Space Center by Energetics Science, Division of Becton Dickinson and

Company under contract NAS 10-9492 during the period October 25, 1978 to November

28, 1979. The contract was entitled "Toxic Level Hydrazine Analyzer Development".

The ES Program Manager and Principal Investigator was Dr. Joseph R. Stetter, and

the NASA contract Technical Manager was Mr. Perry H. Rogers, Technical Represen-

tative, NASA, Kennedy Space Center, Florida.

Acknowledgements for the success of the work performed under this contract

must include the entire ES staff but in particular Joseph C. Delfino, Louis Metzger,

Howard W. Bay, and Sydney Krivin for engineering, design, and documentation of the

prototype instrument which was constructed. Further, this program could not have

achieved its goals without the full support, cooperation, and encouragement of

' Energetics Science management, Mr. Robert E. Lieb, President.

Expert consultations with the NASA Technical Representatives; particularly

Mr. Perry H. Rogers and Mr. Marshall Scott, and the Naval Research Laboratory,

particularly, Dr. Raymond Saunders and Dr. James J. DeCorpo were invaluable during

the conduct of this program.

Page 8: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I I

J:ARY

The space shuttle prr. at Kennedy Space Center will involve the use and

handling of large quantities of hypergolic propellante including hydrazine (H),

monomethylhydrezinn (MMH), and unoytmuetrical diinthylhydrazine (UDMB). Hydrazine.

compounds (H, )*flI, and UH) are highly toxic, and threshold limit values (TLV)

have been established by OSHA at 1.0 ppm H, 0.2 ppm Mliii and 0.5 ppm UDMH.

Original investigations (see references 10 and 11) focused upon the adaptation

of existing Energetics Science technology (U.S. Patents #4,001,103, 4,042,464) for

hydrazines monitoring. This cooperative NASA and Enetgetics Science effort resulted

in successful commercial instrumentation for monitoring hydraines at the PPM level

(Energetics Science U.S. Patent appin. #916,296, NASA case 0 KSC-11082). This

instrumentation however does not meet the current need for a ppb level detector for

MIN.

There are not toxic level hydrazine vapor monitors commercially available

meeting KSC's requirement for a low cost, accurate, reliable and simple to operate

and maintain instrument which can read in the parts-per-billion range.

The objectives of NAS 10-9492 are: 1) to develop electroch'mical sensor

technology capable of PPB level hypergolic vapor sensing, and 2) to design, fabricate

and deliver to KSC one portable instrument capable of meeting the design goals.

A report of the completion of this contract is the subject of this final

report. In summary, the following tasks were completed within the scope of this

work.

Page 9: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

(

TASK I Development of Electrode/Electrolyte/Potential conditions

for the ppb level Hydrazine Sensing Reaction.

TASK II Development of the Electrochemical Cell Design.

TASK . III Complete Design of Instrument Electronics.

TASK IV Complete Design of Instrument Hardware.

TASK V Fabrication and Evaluation. Testing of Hydrazines Instrument.

TASK vi Evaluation of Instrument Calibration and Hydrazine Handling Techniques for Low Concentration (ppb) of Hydrazine.

TASK VII Delivery of Instrumentation and Documentation.

The prototype toxic level analyzer is the first instrument of its kind that

is capable of performing cost-effective and reliable measurements for PPB level

hydrazine vapors. The prototype toxic level analyzer either meets or exceeds this

prograth required design and performance goals for every category except response

time at the lowest levels.

The permeation tube method of preparation of low concentration of hydrazines

were evaluated and reliability for this technique was established by comparison

with acceptable colorimetric and electrochemical methods.

Results indicate that the electrochemical method is more selective than the

colorimetric method towards Y detection and can be used at lower levels. Cali-

bration of the prototype instrument is recommended to be done with hydrazine mix-

tures in nitrogen as oxidative decomposition of hydrazines in air had been shown

to occur. Further applications of electrochemical sensing technology can be made

in the development of analytical instrumentation for dosimeters and safety moni-

toring of hypergolic vapors.

Page 10: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

- -

-,•1

tMt it ) 3S

t;

I'

r

- - - .- -- :-•' 1',.-.. -J.4't-

2r t 4.-

-- ; --

• -:--- - -: .-----'::•.

-

: I• ,I "

'i:-.: j '_•; :. -1

:

ap LL

10 :

-I

Al

N

ii

C-

•.1•"

• •,.;_-'l •

Page 11: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE OF CONTENIS

lL . PACE

Table of Contents •

List of Tables . . .................................................. ii

List of Figures ................ • ............................ iv

I • INTRODUCTION ..................................................1

II. EXPERIMENTAL .................... .2

III. RESULTS AND DISCUSSIONS .......................................9

A. Membrane ............................................. 10

B. Electrolyte ................................................10

C. Sensors ................................................ 17

D. Optimum Operation Conditions ..............................31

i. Temperature Compensation .............................31

ii. Response Time ........................................34

iii. Saturation ...........................................38

E. Analysis and Handling of Hypergolic Vapors ................38

F. Prototype Instrument ................. 40

IV. CONCLUSIONS AND RECOMMENDATIONS ...............................72

REFERENCES....................................................

APPENDIX I Operation of the Permeation Tube Calibration System 79

APPENDIX II Operation of the Hydrazines Dilution Apparatus .........82

APPENDIX III Analytical Procedures for H, MM and UDMH Analysis 86

APPENDIX IV Circuitry .............................................96

Page 12: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

LIST OF_CABLIS

of

SAGE

TABLE I Design Goals: Portable Hypergolic Vapor Detection Instrument 3

TABLE II Instrument Performance Goals ............................... 4

TABLE III Evaluation of Membrane Performance ......................... 11

TABLE IV Evaluation of Electrolyte Impedance ........................ 13

TABLE V Electrolyte Evaluation on H.P. Gold 0 0.000 Volts vs. Pt/Air Reference ................................................... 14

TABLE VI Stability of 10% KOR, 22 Gel Electrolyte ................... 15

TABLE VII Long Term Zero and Span Stability Towards MMII Using 23% KOR, .25% Gel as Electrolyte .................................... 16

TABLE VIII Evaluation of Different Types of Electrodes Materials for Sensor Performance ......................................... 18

TABLE IX Electrochemical Characteristics of Standard and High Purity Gold Electrode Sensor ...................................... 19

TABLE X Performance of a High Purity Cold Working Electrode (EXP-EHP-1) Sensor .............................................. 20

TABLE XI Electrode Loading Study 0.000 Volts vs. Pt/Air Reference In Gel Electrolyte ............................................ 22

TABLE XII Specificity as a Function of Electrode P,tential ........... 23

TABLE XIII Effect of Flow Scheme on Instrument Response ............... 25

TABLE XIV Hydrazine Sensor Response. Magnitude at Various Flowrates ... 27

TABLE XV Hydrazine Sensor Response Time at Various Flowrates ......... 29

TABLE XIV Hydrazine Sensor Response Magnitude at Various Flowrates ... 36

TABLE XVI The Relative Instrument Response Ratio for H, MMH, and UDMH 39

TABLE XVII Short Term Stability of the Permeation Tube ................ 41

TABLE XVIII Long Term Stability of the Permeation Tube ................. 42

TABLE XIX Operating Controls and Indicators of the Prototype Hydrazine Analyzer ................................................... 47

ii

Page 13: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

LIST OF TABLES (Continued)

PACE

TABLE XX Prototype Toxic Level Instrument Design Specifications ...... . 59

TABLE XXI Prototype Toxic L'vel Instrument Performance Characteristics • 60

TABLE XXII Interference Equivalents of Selected Pollutants .............. 63 TABLE XXIII The Prototype Toxic Level Analyzer Relative Response Ratios

For H, MMH and UDMH .......................................... 67 TABLE XXIV Comparison of Electrochemical and Colorinetric Method for the

Determination of Hydrazines in Air and in Nitrogen ........... 69 TABLE XXV Comparison of the Prototype Toxic Level Analyzer Response to

MMHin Air and in Nitrogen .................................... 70 TABLE XXVI Design Goals Portable Hypergolic Vapor Detection Instrument 74

TABLE XXVII Instrument Performance Goals ................................. 75

iii

Page 14: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

FIGURE 1

FIGURE 2

FIGURE 3

FIGURE 4

FIGURE 5

FIGURE 6

FIGURE 7

FIGURE 8

FIGURE 9

FIGURE 10

LIST 'OF FIClI 3

PAGE

Schematic of Electrochemical Sensor .........................6

Potentiostat and Sensor Electrcdes .........................

Flow Diagram for the Toxic Level Inst ruze... .................

Hydrazine Sensor Response at Various Flowrates ..............28

Hydrasine Sensor Response Time at Various FFwracs .........30

Long Term Instrument Zero and Span Drift Measured vlith Filtered Laboratory Air .....................................32

Instrument Response Magnitude and Zero Drift at Various Tern-p-atures ...................................................

Response to Changing Concentration (MMII) .....................35

Linearity of the MMII PPB Level An...lyzer .....................43

MMII Response for Prototype Toxic Level MMII Detection Instru- ment ........................................................45

Prototype Hydrazine Analyzer ................................46

Prototype Hydrazine Analyzer - Intern-1 layout ..............48

Schematic Flow Diagram fr the Prototype Toxic Level Analyzer Measurement Pri1Lcipl .......................................5)

Schematic Electronic B1ok Diagram fur the Low Level MMII Detection ..................................................51

Precision Study of the Prototype Toxic Level MMII Analyzer ... 53

Linearity Study of the Prototype Toxic Level MMII Analyzer ... 54

Prototype Toxic Level Analyzer Sensor and Instrument R.sponse Magnitude at Various Temperature ............................57

Prototype Toxic Level Analyzer Zero at Various (Normalized vs. Scnsor Output @ 24°C) Temperature .......................5

FIGURE 11

FIGURE 12

FIGURE 13

FIGURE 14

FIGURE 15

FIGURE 16

FIGURE l•i

FIGURE 18

on

FIGURE 19 Remote Sampling Pro..e A3sembly .............................. 65

FIGURE 20 Effect of Remote Sampling P'obc on MMII Response .............

FIGURE 21 Comparizon of the Prototype Toxic Level Analyzer Response to }4 Li Air and in Nitrogen .................................. '1

FIGURE 22 Prototìpe Toxic Level Analyzer .............................. 73

iv

Page 15: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I

S S

I. INTRODUCTION

The Space Shuttle program at Kennedy Space Center will involve the use and

handling of large quantities of hypergolic propellants including hydrazine (H)

mononethylhydra&ina (IM), and unsymmetrical dimethylhydrazin (UM). The toxicity

of these compounds is well known and current recommended exposure levels (ILV) are

0.1, 0.2 and 0.5 ppm V/V in air for H. eOI, and UDO, respectively (1). Skin and

respiratory exposure can yield a wide variety of effects, from nausea to carcinomas

(2).

Methods for determination of these three hydrazinea (H, *CI and UDIUl) include

colorimetry (3,4), titration with standard potassium iodate solution (5), an acid-

_'. method (6), gas chromatography (7), derivative chromatography (8) and chem-

tiusinescence (9). However, these methods are not widely used, since they suffer

from various drawbacks such as complexity, insufficient sensitivity or lack of

portability of the instrumentation (making them not easily adapted for use in a

field instrument).

An electrochemical cell has been developed which, when coupled with an instru-

ment system, can provide fast, accurate, sensitive and reaI-time determination of

OO4. H and UD)Oi vapors at ppb levels.

This final report covers work performed under contract NAS 10-9492 for the

period October 25, 1978 to November 30, 1979. The objectives of NAS 10-9492 arc:

1) to develop electrochemical technology capable of PPB level hypergolic vapor sen-

sing and 2) to design, fabricate and deliver to KSC one portable instrument meeting

the design goals. The objective of this report is to summarize the major findings

of this work.

Page 16: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

Two prior reports (10 11) detail the electrochemical technology which was

used to develop the fid inotallatton and pc-rtable instrumentation for hydrarines

sensing. A oLilar approach has been taken in this program for the development of

instrentatLoa capable of sensing in real-time at the ppb level.

In stry, the following tasks were completed within the scope of this work:

TASK I Development of Electrode/Electrolyte/Potential conditions

for the ppb level Hydrazine Sensing Reaction.

TASK U Development of the Electrochemical Cell Design.

TASK III Complete Design of Instrument Electronics.

TASK IV Complete Deei,n of Instrument Hardware.

TASK v Fabrication and Evaluation Testing of Hydrazine instrument.

TASK vi Evaluation of Instrument Calibration and Hydrazine Handling Techniques for low Concentration (ppb) of Uydrine.

TASK VII Delivery of Instrumentation and Documentation.

The design and performance goals for the portable PPB instrumentation for MM are

given in Table I and Table II respectively.

The following report discusses the effort necessary to meet these instrument

design objectives and successfully complete the major tasks of thin work.

II. EXPERIMENTAL

The fundamental design of these instrtuu'nts include an electrochemical cell

as the vapor detector. A complete description of this technique has

been reported (10, 11) and therefore only a summary of the experimental techniques

use4 for development of the instrumentation is discussed here.

2

Page 17: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I CONSTRUCTION:

TABLE I

DESIGN GOALS PORTABLE HYPEUGOLIC VAPOR DETECTION INSTRUMENT

GOAL

Portable, Single Readout of

Hydrazine Vapor Conc. in Air.

Sensor responds to all Hydrazine types (LI, O4R and UDMH), but need

not differentiate between them.

0-2 PPM with 1 PPB resolution.

0.05 PPM minimum detectable cone. readabla to t 1 PPB.

0-40°C.

l0-95Z.

8" x 8" x 16".

'12 lbs.

Iigitat, readable in sunlight 3 digit resolution. Also provide a recordmr output.

Kuggedized, hazard proofed. insen-sitive to changes in position.

hattery, 8 hours continuous, with rovision for 105-125V AC power/

recharge jack.

Audible alarm and light alarm, •-justable trigger level.

INSTRUMENT TYPE:

SPECIFICITY

RANGE:

I SENSITIVITY:

TEMPERATURE RANGE:

RELATIVE HUMIDITY:

DIMENSIONS (Maximum):

WEIGHT:

READOUT:

Iftme

3

Page 18: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

RESPONSE TIME (to 90% of

reading change at 0.1 PPM

or above):

ACCURACY (at 0.1 PPM or above):

PRECISION:

ZERO DRIFT:

SPAN DRIFT:

NO! SE:

INTERFERENCES:

TABLE II

INSTRUMENT PERFORMANCE GOALS

COAL

30 seconds

±10%

± 1% F.S.

< 1% F.S. per day

< 1% P.S. per day

± 1% P.S. per day

The following gases will give the

interference ratio shown or great-er:

INTERFERENCE RATIO COAL

100:1

100:1

1,000:1

1,000:1

No Response

.1

GAS

NH3

NO2

FREON

CO

N21 02, H2, Ar, He, CH4 and CO2

4

Page 19: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

A schematic diagram of the electrochemical sensor design is shown in Ftgur4 L

The three electrodes are all Teflon-bonded diffusion electrodes prepared by fabri-

cating the catalyst onto a hydrophobic Teflon film. The platinum and gold catalyst

used were of high purity. These electrodes were sealed inside a polypropylenechamber

which was subsequently filled with electrolyte. The alkaline gel electrolyte was

prepared from regent grade materials and distilled water.

Gold and platinum leads from the sensor electrodes were attached to a potenti°

stat (Figure 2) and hydrazine sensing electrodes were potentiost0tiCalY controlled

at 0.000 V with respect to the Pt/Air

refereIce electrode. The reference electrode,

Pt/Air was stable to ± 0.OlV at approximately 1.0 ± .OlOV in basic electrolyte with

respect to the normal hydrogen electrode.

The hydrazine cells used 0.25% gel, 23% Koii solution as electrolyte. During

sensor evaluation, hydrazine mixtures were passed over the back (gas) side of the-

sensing electrode at constant flowrate, typically 400 cc/mm. and the current pro-

duced by electrochemical reaction in the sensor flowing between the sensing and

counter electrodes was monitored. The sensors currents were measured by monitoring

the voltage drop across a precision resistor (typically 1K) in series with the

sensing electrode and displaying this voltage on a LCD. Background currents were

measured for the sensor in a 'static' condition (no gas flow through the Sensor)

and in a dynamic vs "steady state" condition, i.e., with a constant gas flow of

Zero grade air (79% N2, 21% 2) through the sensor. Signals for the various gas

mixtures ( 2 ppm }il0{) were obtained directly from the permeation device gas out-

let or from a sample bag for higher tm concentrations by using an air sampling

pump, drawing the gas into the sensor at flowrates which were constant for each

analysis. In this manner the sensor signal (current) was measured as the differfl

In sensor output at steady-state between zero air and the pollutant gas miturs.

FL 2627 WSMCIPMET TECHNICAL LIBRARY VANDENBERG AFB CA 93437-6021

5

Page 20: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

LI

0

rn

'-4

Cl)

NOW

r.

H

Page 21: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I

U

+ I

$1

•1

C) C

r T71 I I •

II tv C, I

L

C) 0 C

m

rn C-

C) '-3

C)

Cli

mz -3-'

7

Page 22: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

A permeation tube calibration system (Model 670 Kin-Tek Precision Calibration

System) was used for continuous generation of hydrazines vapor mixtures between

0.010 PPM and 2.000 PPM, The system operates by maintaining a constant tempera-

ture at which a permeation tube emits a known weight of the vapor at a constant

rate into a diluent stream of 99.9998% N2. N2 was most frequently used as the

diluent since hydrazines vapors were found to be more stable in N2 than air..

A controlled flow of the diluent gas passes through a preheating chamber

which is used to warm the gas to the same temperature at which the tube is thertno-

statted. It then passes through the permeation tube glass chamber where it picks

up and mixes with the vapor. The blended vapor then exits the system and is

connected directly to the analyzer via a manifold which allows venting of excess

calibration gas through a scrubber. By the temperature control, number of per-

meation tubes used, and by adjusting the flowrate of diluent gas, a variety of mix-

tures from 10 ppb - 2000 ppb can be generated. For a detailed procedure for the

set up and operation of the permeation tube calibration system, See Appendix I.

The dynamic dilution apparatus as described in a previous report (11) was

used to synthesize high concentrations (> 2 ppm) mixtures of Hydrazine, MM and

UDMH in both N2 and Air. For a detailed procedure for the operation of the dilu-

tion apparatus, See Appendix II. Whenever possible available standard gas mixtures

were obtained, for NO/N2, NO2/Air, H2/Air, CO/Air, NH3/N2, H2S/N2, S02 /Air, C2114/Air,

Freon-12/142 samples, mixtures were obtained commercially at various PPM level con-

centrations, while CO 2 , N 2 , 0 2 and Air were obtained as pure gases.

The permeation tube method of preparation of low concentration

was evaluated for its reLiability by comparison with the established specific

colorimetric method. Vapors emitted from the per'eation tube at 60°C were cr.Ilccted

8

Page 23: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

- -

for 2 hours into a midget impinger. Hydrazine vapors were collected in O.1N HC1,

in a Citric Acid/N52 HPO4 buffer solution. }H vapors in 0.1N H2SO4 and UDO3 vapors

As the detailed procedures have been reported previously (11), only a brief summary

will be described here. For the detailed procedures. See Appendix III, A,BC.

The analyses of aqueous samples of hydrazine and )O involves the reaction with

p-dimethYl aminobenzaldehyde to form a yellow dye, for UflI, reaction with trisodiU

dimethylamifloPentYan0fte to form a red solution. The concentrations of the

hydrazines were determined colorimet1c13UY at a wavelength of 457 nxn for N2H4 and

!1H, and at 500 us for UDME. Standard solutions of H, M*I and UH were prepared

gravimetricallY from the appropriate salts of the hydrazine compounds. Calculation

of the emission rate in nanograma per minute from the colorilnetry yields results in

excellent agreement with those specified by the permeation tube manufacturer.

RESULTS AND DISCUSSIONS

For the purpose of clarity, this section of the report is divided into the

following sections:A. Membrane

B. Electrolyte

c. Sensors

D. Optimum Operation Coiditions J. Temperature Compensation

ii. Response Time

iii. Saturation

S. Analysis and Handling of HypergoliC Vapors

F. Prototype Instrument

9

Page 24: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

A. MEMBRANE

The initial phase in the development of this instrument was the evaluation of

the differunt types of diffusion membranes. Electrochemical cells we.s constructed -

using different types of diffusion membrane numbers EX-122, EX-Ql, EX-10 and their

suitability determined. A diffusion membrane must possess the following properties

in order to optimize the MM sensors response:

a) Ruggedness, b) copatibility with electrode, c) high permeability, d) 1,w

evaporation, i.e., little water loss from the electrolyte.

An experimental sensor membrane electrode was evaluated for ruggedness by

manufacturing several HF design sensors filling them with free KO}I and gelled KOH,

placing then at -SC and subsequently dropping them from heights of 8 ft. None of

the sensors included in this test failed due to rupture of the membrane. Increas-

ing the dropping height to 15 ft, the EX-122 membrane electrode failed the rugged-

ness test and the membrane was ruptured. Further tests to evaluate the suitability

. of the membrane indicated that the EX-Q1 membrane gave the optimum overall perfor-

mance; hence all further electrodes were made using the EX-Qi. membrane. The results

on the membrane evaluation are suarized in Table III.

B. ELECTROLYTE

An electrolyte must possess the following properties to be useful in our ppb

level MM detection sensor: a) stability - biological, chemical, b) compatibility

with electrode, c) non reactivity at potential employed, d) conductivity.

In the initial phase of this program, ten electrolytes were prepared and

evaluated as potential electrolytes for the sensor system. A special conductivity

cnII was constructed for evaluation of the electrolytes. Their contribution t'

the electrochemical cell conductivity was measured using a YSI Model 31 conduc-

tivity bridge. All chemicals were reagent grade where possible and all solutions

10

Page 25: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

WI. LOSS on 0% RH (GR.Afl/DAY)

0.60

0.30

0.86

TABLE III

EVALUATION OF MEMBRANE PERFORMANCE

TYPE TENSILE STRENGTH

(ZITEI (1b/inch widthl

G-Q1 3.1 - 4.1

G- 10 5-6

606-122 .6 - 1.2

UA/PPM bm

12.0

6.0

8.0

11

Page 26: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

were made using triply distilled water. Table IV shows the approximate con-

tributions using a Model 6956 type electrochemical cell of various electrolytes

to the overa.i cell Impedance. Halide salts were not stable for even short

periods but K2CO3, KHCO3, and the usual KOfi exhibited the most promising be-

havior.

These electrolytes were further tested for selectivity towards MMII detection.

KOR exhibited the most favorable behavior in terms of signal stability and

specificity towards IM. K2CO3 electrolyte does not offer good selectivity with

respect to NO, NO2 , NH3 or SOS, and signals obtained for MM with H2SO4 electro-

lyte deteriorated to less than 10% of their initial value within 24 hours. Table V

starizes the electrolyte evaluation in terms of signal stability and specificity

towards HM.

In order to develop attitude insensitive HF design sensors, gelled KOH elec-

trolytes were used. These sensors were evaluated by operating them in various

'. positions while sampling MMII. No change in signal magnitude or response character-

istics were observed over the 15 minute sampling period used in the ex'eriments.

The short term stability of two 10% KOR gel senso-s was determined after one month

of intermittent use. MMII signals did not change appreciably but response times and

selectivity improved with time ea shown in Table Vi.

However, in continuous monitoring for 8 hours, the sensor with 10% KOH, 2%

gel electrolyte lost its sensitivity due to 'skin' formation on the electrode sur-

face. This is mainly due to the drying up of the gel at the electrode .hih then

causes the conductivity between the electrode and electrolyte to drop signiiic1it1v.

In order to bypass this evaporation problem, a 23% KOH with 0.25% gel electrolyte

was used. Its 'superior' improvement as referenced to long-term stability is in-

dicated in Table VII. For approximately 100 hours of continuous monitoring, the

MM signal has only varied by less than 10%. From the long-term stability under con-

tinuous use and its attitude Insensitive response, the 23% KON with 0.25% gel was

chosen to be the electrolyte used for the ppb MMII analyzer.

12

Page 27: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE IV

EVALUATION OF CTROLYTE INPEDANCE

ELECTROLYTE

CONTRIBuTimi TO Tv{E IMPEDANCE OF

)DEL 6956 ELECTROC11EMIGL CELL - O1fl -

5.ONKOH<2

1.ONKCL15

2.0 N 1138032100

1.0NK.Br15

1.0NNBC120

1.0 N K2CO321

1.0 N LLC126

0.6 N Na2B40287.4

1.0NKNO319

1.0 N NaNO323

1.0NNaNU2 122

13

Page 28: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE V

ELECTItOLY1E EVALUATION ON H.P. COLD @ 0.000 VOLTS VS. Pt/MR REFERENCE

• 20% K2C(. 3 28% 112S0,

SIGNAL OR CNALOR - _IERcFEQuiV. .INE'vRN ;E EQUIV.

1-b UA 0 V

1.8uA OpA

1.3 iA 0 tM

4.7 t;./ppm *33 lilt/ppm

25,23:1 NONE DETECTED

193:-1 233:-i

332:1 ,081:1

4.3:1 65:1

0.3:1 I 6:1

GAS

Zero Air (Static)

Zero Ai (Dynamic)

N2

0.15 ppm t'Q!

1000 ppn CO

12 ppm NO2

50 ppm NH3

23.5 priNO

20.5 ppri 502

23% KOR

• SIGNAL OR N''rERJcc EQUIV.

0.1 VA

0.1 uA

0.1 hA

11.8 h'A/ppm

1,5OO:1

1,20o:-1

3,278:1

4ONL ITECTED

DETECTED

* ?*IH signal drops to 0.1 pA/ppm after 24 hours.

14

Page 29: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE vi

STABILITY OF 101 KOH 21 GEL ELECTROLYTE

GAS __________ EHC1

SZAL OR INTERFERENCE EQUIV. SIGNAL 09 INTERFERENCE EQUIV.

3-19 4-19 3-19 4-19

Zero Air (Static) 0.9 iiA 0 uA 0.2 VIA C u.\

Zero Air (Dyn.atc) 0.9 pA 0 pA 0.2 ph 0 uA

N2 0.9pA 0 p 0.2 VA 0 u

0.15 ppm P90 6.7 pA/ppm 7.5 pA/ppm 3.7 pA/ppm 3.5 pA/ppm

1040 ppm CO, 5,098:1 16,25011 5,728:1 20.222:1

38.4 ppm NO2 927:-i 1,309:-i 939:-i 1,315:-1

50 ppm NH3 3C3:1 5,357:1 141:1 2,18K'1

23.5 ppm NO NOT DETECTED NOT DETECTED 288:1 NOT Dt'Tt(itfl

20-5 ppm S02 350:1 NOT DETECTED NOT DETECTEDt NOT NTtCT1

ppm Freori-12 NOT DETECTED N0 DETECTED NOT DETECTED NOT DETECT) P

SOX 002 NOT DETECTED NOT DETECTED NOT DETECTED NOT DETECTEI)

2931 ppm HZ NOT DETECTED NOT DETECTED NOT DETECTED NOT DETECTU

TIME TO 902 SIGNAL TIME 10 901 S1CN,I.

3-19 4-19 3-19

0.15 ppm P*4 L_. 180 Sec. 80 Sr. 220 Sec.i

* Intermittent use for I Pluoth P 0.000 Vo l ts v. ri IA it ttrt'.

15

Page 30: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TASI.E VII

LONG TERN ZERO AND SPAN STABILITY TtV1ARDS PNH USING 23% KOH, .25Z GEL AS ELECTROLYTE

LCD DISPLAY HOURS ZERO (DftI(p) P4)04 (pp),

0 0 291

24 13 322

48 4 295

96 8 290

so

16

Page 31: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

C. SENSORS

U

In the initial phase of this program sevral types of experimental electrode

materials were fabricated and tested for improved background and signal specificity

characteristics. Table VIII summarizes the performance of these cells. Rhodium

nickel and OLiver electrodes did not exhibit good selectivity towards NO2. Further.

the high 1,A/ppm 10M signal, high signal to background ratio, ease of fabrication,

and extensive prior experience with the gold electrode, lead us to choose gold as

the electrode material.

Gold Electrodes

Two types of gold electrodes were used to test electrode performance, namely.

standard (as in previous sensors) (10,11) and high purity. Table IX shows the re-

sults of these cells, one with a standard Au electrode and two experimental elec-

trodes of high purity Au. The two high-purity gold experimental cells were more

selective under the experimental conditions then corrcsonding standard gold elec-

trode as indicated by their much rger interference ratios for co, NO2, and 110.

To determine if the selectivity ri..io observed with the high purity gold electrode

is reproducible, several samples of the experimental high purity Au used for the

experiment were prepared. Results are summarized in Table X for an electrode po-

tentiostated at O.00V vs the Whir reference electrode. Excellent selectivity is

again observed for all gases except H2S, which always gave an equivalent signal to

104H.

Since h'gh purity gold electrodes fabricated otitts a rugged Teflon membrane l'av'

been established to offer the most promising results for use as ppb level

later efforts have been placed on optimization of this system. In an attempt to

improve the response characteristics of the electrochemical sensor towards low

level hydrazine detection, a study of the effect of the catalyst loading was ni-

dertaken with special emphasis upon response time. Electrode catalyst loadings of

17

Page 32: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

Electrolyte: 232 KOH Potential. No Pt/Air): O.000V

ELECTRODE

6.91 14.79

9.6 13.5

9.4 12.0

9.2 15.5

NOT DETECTED 135:1

NOT DETECTED 1842:1

-3:1 -4.5:1

0.67:1 1.1:1

NOT DETECTED 37:1

NOT DETECTED 5.5:1

12 sec. 81 sec.

15.7

-0.8

2.4

13.6:1

303:1

-8.3:1

0.98:1

180:1

386:1

9-11 sec

2.2

7.2

7.2

55:1

2157:1

-6.9:1

TABLE VIII

EVALUATION OF DIFFERENT TYPES OF ELECTRODES )&TERLALS FOR SENSOR PERFORMANCE

GAS/VAPOR CONCENTRATION TESTED

7.0 ppm MFui/N2

(u&/ppm)

Zero Air Static WA)

Zero Air Dynamic (uA)

Pure N2 OA)

50 ppm NH3 (ppm9H)

1000 ppm CO

40 PPm NO2

26 ppm H2S/N2

23.5 ppm NO/N2

20.5 ppm S02/N2

Rise Time (902 at 7 ppm ?*0i)

Nwe

18

Page 33: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

S I

TABLE IX

ELECTROCHEMICAL CHARACTERISTICS OF STANDARD AND

-, HIGH PURITY GOLD ELECTRODE SENSOR

CELL SIGNALS'

GAS/VAPOR CONCENTRATION

Au-i2 Au-23 TESTED

BIAS MV BIAS MV 0.00 0.00 -

7.0 ppm P4R/N2 15.7 1.9

jA/ppm

ZERO AIR - A -0.8 1.3

PURE N2 - *A +2.4 1.3

50 PPM NH3/N2 13.6:1 32:1

1000 ppm CO/Air 303:1 94,500:1

40 ppm NO2/Air -8.3:1 -1,454:1

8 ppm NO/N2 180:1 NO SIGNAL

25 ppm S02/Air 386:1 33:1

25 ppm H2S/N2 0.98:1 0.9:1

ALL THE RATIOS IN THE TABLE ARE: PPM GAS/PPM 0fH

2 Au-1 Membrane: 606-122, Electrode: SID. Au

Au-? Membrane: 606-122, Electrde E)P-W'-AU

' u-1 = Membrane: 606-123, Electrode E.P-HP-AU

Au-HIAS MV

0.00

8.5

0.52

0.51

64:1

47. 333:1

-1,639:1

NO SIGNAL

NO SIGNAL

1.6:1

19

Page 34: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE X

PERFORMANCE OF A HIGH PURITY GOLD WORKING ELECTRODE (EXP-EI!P-1) SENSOR

SIGNAL OR TIME TO

GAS INTERFERENCE RATIO 90% RISE

Zero Air (Static) 3.3 IjA (-0.5)'

Zero Air (Dynamic) 3.4 iA

7 ppm )2H 7 ppm 10.5 Sec

0.15 ppm HM 0.15 ppm 150 Sec

206 ppm CO 14,237:1 (12500:1)1

23.5 ppm NO 219:1 (not detected)'

38.4 ppm NO2 -1,196:1 (1450:1)'

50 ppm NH3 142:1 (945:1)'

20.5 ppm SO2 18:1 (not detected)'

26 p.m H2S 0.8:1

1160 ppm Freon --- (not detected)

502 CO2--- (not detected)'

2931 ppm H2 - ---- (n,t detected)'

1) Performed at potential 150 my lower.

20

Page 35: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

1.2, 2.5 and 5.0 mg/ca 2 were evaluated. The results in Table XI indicate that the

response to 1.1 ppm MMH was optimized at 45 seconds to 90% with 2.5 mg/cm 2 catalyst

loadings.

To further establish the optimum operating conditions for the high purity gold

electrode, the electrochemical specificity was studied as a function of potential

settings. Table XII is a stary of the results based on the typical response of

eight sena(.TB. (.'otimum specificity is obtained at a potential of 0.000 Volts vs the

Pt/Air reference in our gel. electrolyte. This potential has then been selected for

use in all subsequent prototype instrumentation testings.

In order to improve the sensors' lifetime, i.e., minimize the rate of evapora-

tion, and to improve the response characteristics of the electrochemical sensor, a

new configuration of the electrodes is employed. Figure 1 illustrates the new .on-

figuration. This new configuration minimizes the distance between electrodes and

therefore maximizes response parameters. In addition, the new sensor configurations

will be virtually attitude insensitive. It is also observed that improved response

characteristics are obtained when the sample is pulled through the sensor and

plumbing before the sensor is as short as possible. (See Table Xlii for results).

Figure 3 is a modified flow diagram of the flow scheme which is incorporated into

the final instrument design.

The steady-state current response of the high purity gold electrode was measured

at various flowrates between 0 and 700 cc/min for MMH/N2 for two different elec-

trode sizes. Results are summarized in Table XIV and shown in Figure 4. It is ob-

served that the sensitivity of the device diminishes rapidly at flowrates below 400

ml/min as does the instrument response time, (See Table XV and Figure 5), therefore,

400 ml/mm was selected as the operating flow of the instriimcnt.

21

Page 36: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE 41

ELECTRODE LOADING STUDY •0.000 VOLTS vs Pt/Air REFERENCE IN GEL ELEeTROLYTE

-.

1.2 rrqicm 2.5 mg/cm 5.0 mg/cm-

SIGNAL OR SIGNAL OR SIGNAL OR

INTERFERENCE INTERFERENCE. INTERFERENCL

GAS - EQUIVALENT EQUIVALENT EQUIVALENT -

ZERO (STATIC) 0.05 vA 0.10 pA 0.90 IAA

ZERO (DYNAMIC) 0.10 VIA 0.20 pA 0.45 pA

1420.20 pA 0.50 pA 1.00 pA

1.1 ppn PiI 14.3 pA/ppm 12.89 pA/ppill 16.56 pA/ppm

1040 ppm Co 28,000:1 15,917:1 9,383:1

, 9 ppm NO2 • 315:-i 659:-i 923:-i

23.5 ppm NO NOT DETECTED NOT DETECTED NOT DETECTED

50 ppm NH3 3,750:1 1,684:1 358:1

21.5 ppm SO2 . NOT DETECTED NOT DETECTED 231:1

RESPONSE TO 90% 75 SEC. 45 SEC. 90 SEC.

22

Page 37: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

is I: TABLE xi

SPECIFICITY AS A FUNCTION OF ELECTRODE POTENTIAL*

....ft wwi vm Yt ...fl lflfl flhl Irc fl flflfl UnITC efl Inn VIM TC 4 fl 9flfl VflI T

GAS

SICLL OR IN CE

EOJIIYLT

SICAL OR INTKFERENCE EQUIVALENT

SIGNAL OR INTERFERENCE EQUIVALENT

SIGNAL OR INTERFERENCE EQUiVALENT

SIGNAL OR INTERFERENCE EQUIVALENT

ZERO

-

(STATIC) -. 2.08 pA - 0.30 pA 0.01 pA 0.55 pA 1.08 pA

ZERO (DYNAMIC) - 2.20 pA - 0.30 pA 0.03 pA 0.59 pA 1.21 pA

N2 -O.30pA -0.20pA 0.17pA 0.69pA 1.34pA

1.10 PPM 9.63 pA/ 13.97 pA/ 15.96 pA/ 18.21 pA/ 13.43 pA/ MMH ppm ppm ppm ppm ppm

1040 PPM CO 79,561:1 64,961:1. 35,519:1 57,016:1 61,602:1

¶ç,M NO2 102:-1 . 367:-i 11460:-i 9,319:-i NOT DETECTtD

50 PPM NH3 NOT DETECTED 31,475:1 . 4187:1 533:1 1,398:1

23.5 PPM NO NOT DETECTED NOT DETECTED NOT DETECTED 463:1 101:1

21.5 PPM S02 NOT DETECTED f)T DETECTED NOT t)ETECTED 74:1 11:1

* Potentials are listed with respect to the Pt/Air reference electrode.

MW

23

Page 38: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

it .I

' r •i

-I r -I

24

In

rn

rn

rn

vo

Page 39: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE tIII

- -E7CT OF PLOW SCNE ON INSTRUMENT RESPONSE -U

FLOW SCHEME

Push thru sensor (Pump before)

P.fl thru sensor (Pump after)

lot 1CO ppb UI SAMPLE 2nd 100 ppb flI SAMPLE

> 600 seconds 150 seconds

130 seconds 95 seconds

(All response ties noted are as time to 902 of final signal).

['1

-

25

Page 40: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

11

C)

-I

tvi

I.-C)

tTl

6.4 z

.4

ri z

V V

2

• /

Page 41: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE XIV

( HYDRAZINE SENSOR RESPONSE MAGNITUDE AT VARIOUS FLOWRATES

ELECTRODE GEOMETRIC AREA

FLOWRATE 0.50 cui2 1.33 cm

(cc/min) (UA/PPM)* (/PPM)*

50 2.0 4.2

100 2.2 5.9

200 2.5 6.7

400 2.6 8.6

700 2.8 9.5

Response Time (90% Rise) 72 Sec. 105 sec.

Electrode: High Purity Gold.

Electrolyte: 10% KOH, 2% Gel.

* Average Of two separate measurements.

27

Page 42: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

ELECTRODE AREA

0 100

FIGURE 4 HYDRAZINE. SENSOR RESPONSE AT VARIOUS FI.OWRATES

10

9

8

7

SICNALONC

(p A/PPM)

6

4

3

Page 43: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE XV

HYDRAZINE SENSOR RESPONSE T [ME At VARIOUS FL&V,'RATES

RESPONSE TIME

FOWRA't (cc/th) SIGNAL (iA) (901 RISE)_---- -

50 282 16

100 391 31.5

200 48.12 24

400 56.3 14

800 61.4

1000 62.4 12

29

Page 44: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

ill

am

p-.,J

i

'S rooa

Page 45: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

In order for this device to be useful for field measurements the instru-

ment must be able to possess environmental stability. That is, the instrument must

retain ita sensitivity and accuracy over long periods of time and exhibit minimum

sensitivity to fluctuations in ambient conditions. The zero and span drift of a

typical ppb level MM analyzer was monitored over a 23 test day period and the re-

sults are sumsarized in Figure 6. For breadboard instrument prototype, the zero

and span was monitored intermittently for the first 12 days, both zero and span

drift by no more than ± .02 ppm. At day 15, the instrument was put on continuous

testing for zero and span drift, aftet 72 hours of continuous monitoring, again

the zero and span did not drift by more than .± .02 ppm for MMR concentration of

.288 ppm. Short term fluctuations have not been monitored in this experiment but -

the short term effects of the instrument zero can always be minimized by adjusting

the instrument zero immediately prior to measurements by admitting a sample of pure

air or switching valve to zero position to remove the electrochemically active gases

from the inf lowing sample.

D. OPTIMUM OPERATION CONDITIONS

I. Temperature Compensation

A Tenney Environmental Chamber was used to evaluate performance as a function

of temperature.

The first breadboard prototype model ppb level hydrazine analyzer based on th e

electrochemical oxidation of the vapor was evaluated for the effects of -emperature

over the range of 0 to 40°C. The sensor and instrument output were monitored using

0, 0.23 and 0.66 ppm of )ffl. When cycled between 25°C and 40°C zero shifted up 0.03

ppm and span was 51 higher with both concentrations tested. When cycled between 5°C

and 0°C zero shifted down 0.016 ppm and span was 15Z lower with both concentrthr.-

tested. After cycling, room temperature (25°C) zero was within 0.005 ppm and ;p.vi

was within 2% of their original values. These results indicated the need i.ir ru. •-

mal electronic temperature compensation in phis instrument. (See Figure 7). llowever

after further development of the sensor, this experiment was repeated and different r,-

31

Page 46: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I

Iu.

) I ale

4

4J- .1 •-•:;. • OF tith

REPfl4 Is POOR

-J

0

Page 47: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

SENSOR •(( PN

STANDARD CE/REl(•3 r

SENSOR II f á.714

RICH PURITY1 0.245

CE/RE

250

200

0

100

, .".

STANDARD CE/RE

HIGH PtR i ry o C El RE

5(1

20

15

1)

C,

N

tn

£3

S z u.

IN

FIGURE 7 INSTRUMENT RESPONSE MAGNITUDE AND ZERO DRIFT AT VARIOUS TEMPERATURES

0 10 20 30 40

50

TEMPERATURE °C

TLIPERATURE °C

33

Page 48: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

units- were nut * t iiiI wli I cli appears 1 a ter in th text. . .

II. Response Time

An observation made in the course of a linearity study was that the sensr'

response was more rapid to changes of 100 to 200 ppb thun from 0 to 200 ppb. (See

Figure 8). This indicates that changes near TLV will he detected move rapidly than

would be predicted by the response time specficatLOfl since it is sured as a

change from zero ppm ti. Therefrc, the ahUtty of the uni.t to tcpod to c inAing

problem conditions is better than th resporse time .1 11 woud indicate.

The size of the electrode also tound to affCct the rcponse time (T:iblc XIV).

the sir-

ie-

sponse time is found to decrea se with the size of the e1.ectLode Iio'evet,

nai!oncentratiom ratio (A/ppm' '.lo decreased with the thcrease

in the electrode

size, therefore a compromise of the twc' tac:orS must he weighed and an opti:um elec-

trode area of 1.0 cm2 was cho;e; t. se Lth thIs

The response time as in c.t'd hefte is also dpdefl on tit( , fiowrate of gas

through the sensor(Figutc 5.) t\o c"5 can accaunt for the r'tC ti.e

characteristic ; (1) diftercnL ratS for ;tab shaflt; of steady-t3tC Conditions

.d,or in the electrochemical flC k )

°° P ti en dcc

position in the sampling systCd ro 'au:ti's s .'es due to ad ptin .ind

decomposition can be mi nint zd b USC : a opt I tu' ;'ra te and : I es t samp I e

system volume.- Howeve r even w at I juO cn t cap loved n the ;ph ?t'flI :

sor, response times are Lyp-Lci I. • •' f

Further. i iydraIt1 li ben Ic i e.- lv cr IVt en certain :1.11.115.

therefore an inert materi.,l . ie1on ia.f'2r 1cc. 'cud in I.

'listru. t : f

tern components that co . ' i - ecu :u t iL11C--;r

RiTRft ;cii V tii" THE

oRl(;tNA 1 PA , - is POOR

Page 49: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

cc

go

I-' I-

z

*1

z

z

z

z

Lfl z

In

x

Page 50: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TA B 1. 17 XIV

HYDRAZINE SENSOR BFISPOPSK MACN I TUI)E AT VARIOUS FI.)WR,\FKS

ELE(;TRo: CEOMETRIC AREA

FLOWRATE

(cc/mm) (,/PI'M)* (uA/PPM) *

50 1.0 t.2

100 2.2

200 2.5

400 2.( 8.6

700 2. 9.5

Response Time (907. iso) 72c'c. 105 Sec.

Electrode: High Purity Cold.

Electrolyte: i0 KO! 2% Cc'!.

* Average of two sk p : s ? :i t v :c':3 r, ic'n

RFRCU. 0 .ii OF THE OmGrNAL P..: IS POOR

Page 51: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

o LM 0 C —

14 z - - In I- C

• z 140 In U Z 14 o In

In 14

OF •1_? pOOR.

1.

LE

tA

C

In

0

—4

I-.

In z 0

.J

In

LLI z -4

In

-4

0. 0 0 -4

0

00 C

C 0

0 C

0

Page 52: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

iii. Saturation

To determine the effects of saturating the anai.y?.ei with a high concentration J

of hydrazine, a spill was simulated b y pr"paring o 70% 2 I14/ 30% 7120 mixture in a

closed vessel and drawing the vanors above tiho mixturv. Into the Intake of the instru-

ment. The instrinnent became Iis tan teouo1y oaturated upoa introduction of the sam-

ple and could not be used for further analynis of pptk levels of hythazines for approxi-

mately tao hours after removal of the simple. The c1utrctorisLtcs af the It.strument

were the same after recovery 03 they wro prior to Ito aturatLon, indicating that

if the analyzer were expood to a RpiIi it could be reused with good reliability

after a two hour recovery pet Ind.

The magnitude of the scorer response I s J''ieot on the vapors concentration

and the type of the vapor flow trogh the ;cn;or charhur. Toe relative response of

hydrazine, and UDDI on prb liv int .o'r. iich been ealhratcd with 0.288

ppm of 101H is summarized in (Uah o

E. ANALYSIS AND HANDLING, OF II'fPifRGOLLC VA!OiS

One of the most essential phases ii tbc dovo L':ont of new tecaology is the

development of a successfi I l;'p Ie:ter t. I Lou tic or c techno I ov . in the case

of the hypergolic vapors, the reui r': nu: Is Lor procJuze;.,

field functional tcstth nd field lib:ut .

The calibration of tho M:{ onatr:'cr r.0 .L •s ?CCt0LiOfl u:d analysis of It,

?fi-1 and UDMH vapor mixture ;;td ` ­:ii:

: ;Lfldi rd 0 1 ii a 1 tecliniq no.

A dynamic dilution ;ystt' hoc h'e 0 ;!1od 0 0 ''.'O5 t'rt (Ii) 10

vapor mixtures of hydrazin e . nr vflrazne ad lv::;iet tuI im.thyiivdtazine. The dilution system and i to epei.-i I on .1 IV c'm at I zc \ ppud I x i I

However for ppb level hda7.iue : eci •.' I oti ni . 1 ' i\5:ait di u cusystcm

found to bc inadiu;tt_e. Ti, dr. lv ' '•..u• 11 ;: i''' hvi.

zines has been Kin-Tek's 'eio a j ''t;'i• - ' ih i Ofl (0 1,

sys tern in an operating mode-:l' LI' 'v r' ' '. v in no v:-'.

'I

Page 53: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE XVI

THE RELATIVE INSTRUMENT RESPONSE RATIO FOR H, )OIH, AND UDMH

CONC. GAS (PPM) SIGNAL (pA)

mmH .288 .288

H .254 .269

UD!.flI .250 .108

RATIO*

kGAS :MMH)

1.0:1.0

.944:1.0

2.315:1.0

* Ratio is defined to be the PPM of gas equivalent to the signal of 1 PPM MMII.

39

- 0 I / -.0

1•0 ;

go

Page 54: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

The permeation tube method of preparation of low concentrations of ?'OIH was

evaluated. Over seven days the device output concentration was between 1.2 and 1.8

ppm at 400 cc/min of N2 and short term stability was much better as shown ir. (Table

XVII). For comparison, gas emitted from the permeation tube, at .60°C was collected

for 2 hours into a midget impinger containing 25 ml of O.1ON 11 2 SO4 and analyzed

colorimetrically for IIffl. Calculation of the emission rate in nanograiss per minute

yielded results in fair agreement with those spelfJed by th tube manufacturer.

Table XVIII shows the stability of the permeation tube over a two month period.

Utilizing the permeation tube with varied 142 flows passing over the tube, differ-

ent PPM concentrations of MMII were generated from the Kin-Tek's precision calibra-

tion system in an operating mode where the hydrzines proceeded directly into the

analyzer. Five concentrations were prepared by wsing the thermotatted Kin-Tok per-

meation tube calibration system. The instrument w:is caJlbr'ed with a 115 ppb mix-

ture and measureme.ats were recorded with the more concentrated sample. Y (ppb ?lh

found) was fitted to rh a following least-squares line as a function of X (prb MMII

measured by the instrument):

Y = 101.9 X +3ppb

The standard deviation of the po1nts from the itiie was only ± 2.5 pph which

includes the uncertainties in sam.le proparatios. These results confirm the linearity

of the instrument during low range ML( detection. Single point calibration, t,

therefore, possible without loss in uccwucv (Set' Figure 9). in this range.

F. PROTOTYPE LNSTIWH.ENT

With the optimum operation conditions, most, sensitive sensors, and stable cir-

cuitry established, the prot:utypc'. Ilistrurlo;! t was osembic'd. Its sensor exhibited a

typical background current of 0.7 nA mini.t a sen;; it.v to .MHH of approximately 16

PA/ppm. This indicates a backgVemid signal csaiva LeO to ..mppr'_'xJ.ivate.Lv hO p:'h

[ I.4 I I

OF I L1h

onc,r: .:r I.\'.fl IS POOR.

Page 55: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

LTABLE XVII

SHORT TERM STABILITY OF THE PERMEATION TUBE

41

Page 56: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE XVIII

LONG TERM STABILITY OF flEE PE1MJATE0N rUBE

EMISSION RATE

NO • OF DAYS ERATURF _g/n._

0 62 5.35 1,115

14 62 6.96 1,446

28 61 1..50 937.5

42 62 7.80 1,625

49 62 6.S5 1,427

63 61 G.7

Emission tat' (ng/rni.:)Hrur.cs Coi1.cted

Rate as speC11c!-i by inaniIflcttre

Page 57: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

0 100 200

(%(: (pps 'NH)

.3

- LCD

DISPLAY

PPM NIH)

lu

FIGURE 9 LflEARITt OY THE MM PPB LEVEL ANALYZER

Page 58: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

T

The sensor. h.it . rise t Lnt 'i s'ctnd f s tI t.I a

decay t Ic of M) c' Thtu t's \'l %SS I

of sample gas flow. A t1 eil t'snst' s tO FItN' LO hc ye the Arrvv i ti-

dicates zxposure of the 'nct th

The initial signal NVA tht, simsr Is n:r1 y ts hU the attaiunttnt of

steady—state occurs vinl.y ait.'r eral Iinus.

A picture of th ul t I I'v h\drazitio aalv 'r s'ia tn It,uyo

By reference to Table he coixtroi fu:ct j ons &t tht' runt he

The analyzer is contatwd In t dtrat k' t't:1 I. .\ 1 1 ':'rtt iJustnts, .t

mounted on the front tf ftc Fa:) levol s .I f controls.to tIits l€ft

the LCD display r dot thc- y 1tvl antI t

while the lower l,vel \Y t1N I a R y

switches. Directl y aho' t I i: 1 •. L n:u1.

ALA

display re3dout are c.A41,*,, r,% t hs jtrnn t r S '. .' AL\iI Ei '

right of the d Is la . . t I - j i • p • '''

Jack. A recep tat Le t, %,I . S "11 : z. .

the battery charioy to, •' •. I f-- 'i . S.S5S

extreme right of t ho . .- . . . .. .

and a flow tndt:Lt¼SI.

The flow adj 'at I. . . •..• - -••--'". '- s an;i l y re r. TIn' "of t .S J - LA .• - . .- .

haU t -t I t - • .- : • .- ••- . ..

ure 1. ji rtes ts •,... . .. ,.-

structure and lavout. I . --_. •• • ,. . .. • lit hil f are th T' f Ion . • - • 5 .

lower hi I v conta t:- -

battcr' pacI. p' ,-a

REP'J ' - . . •

flRIGP':\I. p.-.. tS PUU

Page 59: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

Eli

- pJ 0 -

o o 0

Q1'- \' I91UO

1

-4 p.'

ITI

0

C

-U rn

p..

m

-4

-4

z

z

I

Page 60: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

4 OF Ttp

-. 4I

Ij,,4 y DISPLAY c4I

'

i ' '. 'v-..i" .. •.

Lttt1

.y.•c:':4

.4

Ir -Lt\,' Hi

`^-, H-11 , q

1

,

FLC,UK 11 R('11)T'f1'C U' Ai\l R

- . 1 2 3 11

12

I I

I I ALAM •'• •

)•

ç:', ! ; V OF' 1ILF I I' ;!':\J, j'•(

Page 61: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I I

'SABLE XIX

OPERATING CONTROL3 AND INDICATORS OF THE PROTOTYPE 'HYDRAZINE ANALYZER

C)NTKQI. UK INDICATi)R FUNCTION

1. Power Turns pp on and off. Supplies pow to all circuits except potentiostat.

2. Battery Tester Checks battery condition on LCD read,ut.

3. Alarm Light Illuminates when an alarm condition is reached.

6. Function Test checks electronic circuitry 1 alarm light, and horn.

. Display Illumination Brightens LCD readout for easier viewing in darkened areas.

6. Horn "ON/OFF" Switch Used to silence or activate audible alarm.

7. Gas Level LCD Readout Indicates the level of hydratines in parts per million (ppm). (See note below).

8. Span Adjustment Used to calibrate the detector with known concentration of hydrazines.

9. Alarm Set Used to set the level at which the audible and visual alarms will activate.

10. Zero Used for the precise setting of instrument zero.

l. Recorder Output Receptacle Provides power and analog si gnal to stri' chart recorder on O-. volt full scale output.

ZERO Allows "ZERO" Air to pass through sensor to establish Instrument zero.

12. Intake Valve OPER. AAows for sampling ambient *1 and cali-bration.

13. ChargIng Receptacle Used for receiving plug from charging unit.

14. FInw Indicator Green marker pops up to show flow through sensor is activated.

15. IMMU IL.ake Couples with the prose to sample ambient air and remove particulates.

16. Flow Meter Indicates flow past sensor.

?.

Flow Adiostmvnt kegu hi ics flow p:is t nsr.

18. C:i-e Durable, impact res j sr:rtt prtoive in-strument hetising.

NOTE: Since the lntrument can ana lvze H • U1, or UDMU • the LCI) readilig refers to the concentration of the gas for which it is calibrated.

Page 62: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

- I&

,i

• .•. • •; . • :

' . p • - • . • I.i.

•.•..-•'•..-• . • ••

J•4i • .'•

• .•

• / v ••-', • .. •',' .1 - •,

L• •. • •

t.;;t. .. ••• -: -

t. .•..t__.•.•&.•_•• .• r -

,•& • .

(1•

S. •• - •'.• .. ••'- •

• •, t - t - • •

ze

RE1'RC' i vt' 1xIJ IS 100R

Page 63: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

The essential parts of the instrument ate the electrochemical se,,sor (:i

ducer), a pump, electronic control and amplifications circuitry and are iu1u.

schematically in Figure 13. The pump draws the sampled vapor mixture t.hroth'

intake and into the electrochemici sensor constant I lowrate. The sensor the.

analyzes the vapor mixture producing an electric current which is proport.ioo.ii .)

concentration of hydrazine in the vapor mixtures. That electrical current 1" b. i

amplified and displayed on an LCD display showing the level in parts per rtilli.u,

schematic electronic block diagram for the PPB level 2-111 detection is showo I

ure 14. A detailed description for the electronic circuit block diagrsin an

found in Appendix IV. Representative responses at room temperature are shown

Figure 10 for 250 ppb of MI in N2. The circles mark the 90% rise and decay

and these are within 50 seconds of vapor mixture exposure. The precision of

analyses was ± 1% (Figure 15) and both precision and response times were foun

improved at higher concentrations.

The instrument response was determined for several MMII concentrations and the

results are shown in Figure 16. A linear least-square analysis of the data si,:h

dicates that the iastrument response is linear in MIIH concentrition within

mental un.ertafnties in the measurements and y ields a eorre Lit ion ceof f Ic icnt

the 0-2 ppm range. The noise level on the instrument was less than I ppb M11

Studies of the effects of temperature upon the performance of the ECLV.

'rument for hydrazine analysis were carried out in an environmental cl':he.

observed previously (ii) at temperature below 10°C, water vapor and hvdri

condensed in the instrument intake tubing and it was very difficult to obtair,

rate and representative results. Special precautions were taken to utIH.c

dry gas mixtures and exclude room air from the environmental chamber and (h.

level analyzer. The results of these experiments are reported In Figure 1. T

49

Page 64: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

' !VX1I ((J

T( . 1J :1itI.lIl

I-,

mgm

x

z

LTJ H

-_-1L._rJ

-'

----S.. -

,.. !f

\

')t(''&Ll3 POOR

A

Page 65: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

CL f-jo-

in co cc

WCD

05 XE

WLL

UJ cn

CL •1 0—i—

L)cn

hc. UJ

,!.,. i•.

Page 66: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

-i

rmo

b

-I

V

-

Page 67: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

C

(I A

g4

z

go

ES

I-I

0 -4

I.

Page 68: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

.2

SIGNAL

(VOLTS)

.1

0.3 C(4C (F'PM tU)

FIGURE 16 LINFARIIY STUDY OF THE PROTOTYPE TOXIC LEVEL ?'<H ANALYZER

0

1.oi..

.5

SIGNAL

(VOLTS)

_--_---__—_—J-_—__

IREPRO' t t)V THE

ORIGINAL IE IS POOR

y4

/

Page 69: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

ISO

0 U, z 11.2 U,

250

200

100

2()

:-

11

I 0

I

FIGURE, 7 INSTRUMENT RESPONSE MAGNITUDE AND ZERO DRIFT AT VARIOUS TEMPERATURES

SENSOR ppm

STANDARD CE/RE . ppm

SENS)R II J RICH PURITY1 0.245 CE/RE -

0 10 20 30 40 50

TEMPERATURE °C or

I'I•A1IRI- O(

cc

/

Page 70: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

sor output (FIgure 17) e!.J.hl ts only Blight variation I torn 0-20°C hut shows

• variation of 25-35% over the temperature region of 2fl--'4(J'C. More tn:trt.nient t -

ings and data has to be obtained before a proper ternpera1nre ruripettaticn (-,-.ti

• incorporated into the instrent.

Instrument zero changes (Figure 16) of ± 100 pph are observed uri'g thts.-

strument but this poses little ptablem since the lustrurneur can easily be zeroed

the field immediately prior or subsequent to vanor measurements.

The zero and span drift measurements are complicated 0.11ce there is :i slm;il-

taneous time dependence for zero and span drif t occur ri;% long WILL he reope r--

ture measurements. The zero drift of an internttterr.ly o perated pph analyzer •aa

4 ppb over a period of 7 da y s and the span drift was 5Z over the saae pe rl.od.

These drifts are necessarily included in rite reported terlerartir. oeaslIrcr.ents.

From the descriptive Instrument data collected, rho geneaI rni:ent s

fications are given in Table XX and XXi.. Rc compari.aa u th table ' aud II (1.

DUCTION), we note that the design goals of the program cejtlie:a 'ue t

have been achieved. T.t i.s a ie I .iper rant to polu that the :o and 'n

fication giv".n in Table XXJ vaLid under r yp it;i ;nb tut aY tauratu a -

tions . At extreme tempera ur. ccu i"u rerc ard uuar. .'.i a io 'e

as no elearonic tempel' t!Ir.: tS t:.a '. ')'u'rat d . at

this time.

In any field us'. the vu r: dot-.-Cc ..iu.

presence of other 3tI',eu.0 . '_' cuu; :th- --:.'t •.

ment. The interferences thee 10 sc!octad p'i titaat.s f';:

-or are given in Table XXI . T'vuater iLttertre . 0 is

constituents of .iabiint at r :t.,rc'lv. (I,

sensor and hence ia not hoc I:-':.i

'Ulit.

.)lth IN \\ P1 11

iOOd SI'' •:u UtI

'i -Ut dO S1ltI1 14

Page 71: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I-

z

z

a

00

I

0

C

C

C

0 -* p

C•4 ('I - - - - 0 0 0

0 0

JflW1O L3).LSN1 dd/SflO

Page 72: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

L

Nt I

L : '

O1G!\.\L S i?\Jt.)j

Page 73: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE

PROTOTYPE TOXIC LEVEL INSTRUMENT DESIGN SPLCIFICATI0S

INSTRUMT TYPE:

SPECIFICITY:

SENSITIVITY:

ALARNt

TEMPERATURE RANGE:

RELATIVE HUMIDITY:

DIMENSIONS (Maximum):

WEIGHT (includes case and strap):

READOuT:

CDNSTRUCTION:

POW ER:

CURRENT DRAIN-NOMINAL:

Descript Ion

Portable, Single Readout of P1H (H or L)MH) Vapor Concentration in air or diluent gas.

Sensor responds to all Hydrazine types (U Mn and UDM1I), but does not differ-entiate between them. The unit is calibrated for the particular gas of interest.

0-2 ppe with 1 ppb resolution.

Readable to 11 ppb.

Audible horn and visible light, adjust-able trigger level.

0-40.C

10-952 RH (can operate at 0-1002 RH but is designed for extensive service between 10 and 952 RH).

21.cn 30.5 cm x 10 c (8.27 in x 12.0 in. * 3.94 in.)

5.0 kg (11 lbs. .4 or.)

LCD DPM with 311 digits. Recorder outputs provided.

Ruggedired. hazard proofed, insensitive to changes in position.

Battery, 8 hours continuous, with pro-vision for recharge. For an hour total.

OFF. O.00 A t)N, 0.110 A. on (with lull alarm 0.310 A).

59

Page 74: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

REPROPUC! T iT.l'1'V OF THE 1T IS P0'1R

PRI)T1TYPE roxic LEVl:3 s t-L1 1' RiJtA.NC' CA\rRl jt

Vi r r 1 y !tt

rt;pou ' t' 10 1ntt IJ

:t nutesi t. 99— 10O i I

101 ()C:p! Int

Illson :iccu .v i, I

ciIbt.i1i.. n Uet toi at,t tct.'fl

o

± x vp lv -. . I

< r.s. r .3viJv;'Ji

._ . •

'11? tJ tr r L. l. S 'U

I;it

"S, • •&

• I \'

RESPONSE T11{E (to 90 t rtt

change dt. 0. 1 ppv. or

ACCURACY (Hi 0.1 rpm or

PRECiI0N:

ZERO DRIFt

SPAN turr

NOISE:

1NrERFEF.NCES:

Page 75: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE

DESIGN GOALS - PORTABLE HYPERGOL1C VAPOR DETECTION INSTRUMENT

GOAL

RANGE:

SENSITIVITY:

CONSTRUCTION:

POWER:

ALRi4:

Portable, Single Readout of

Hydrazine Vapor Conc. in Air.

Sensor responds to all Hydrazine

types (H. P*H and UDMH), but need

not differentiate between thee.

0-2 PPM with 1 PPB resolution.

0.05 PPM ninimun detectable conc.

readable to t 1 PPB.

0-40°C.

lO-95Z.

3" x 8" x 16".

l2lbs.

Digital, readable in sunlight 3 digit resolution. Also provide a recorder output.

Ruggedized, hazard proofed, insen-

sitive to changes in position.

Battery. 8 hours continuous, with

provision for 105-125V AC power/ recharge jack.

Audible alarm and light alarm, ad-

justable trigger level.

INSTRUMENT TYPE:

SPECIFICITY

TEPU' ERATURE &ANCE:

RELATIVE HUMIDITY:

DIMENSIONS (Maximum):

WEIGHT:

READOUT:

61

Page 76: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

T:\liI , II

I N;I Rrr 1'I:RT i:\t:; OWs

GUAL

RESPONSE TIME (to 90 of reading change at 0.1 PPM or above); 30 seond

ACCURACY (at 0.1 PPM or above): .

PRECISIoN:

ZERO DRIFT:per d3v

SPAN DRIFT: .r day

NO1SIF.S. cr d.iy

1NTF1RENC:ES: ....

IC' shown (C•

CAS5TV NCE T!c GOAL

NH3

No2

F R F. ON

CO

N 2 . (1?, H 2 A

II • t:; .CnI (. •.••.

Lc . •iII1:' fl1!r;iis Poop

Page 77: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE XXII

INTERFERENCE EQUIVALENTS OF SELECTED POLLUTANTS

READING DUE TO

INTERFERENCE RATIO INTERMENT ON NMH

PPM INTERMENT IN PPM

PPM MMH

.288 ppm *fl

46.3 ppm NO2/Air

2931 ppm H2

1015 ppm CO/Air

50 ppm NH3/N2

• 46.6. ppm NO/N2 - - -

21.5 ppm S02/N2

902 ppm H2S

• lo,ppm 2

1060 ppm CO2/Air

1160 ppm Freon-12

Air

19.4 ppm C2H4/Air

.288

.008

.002

.012

<.019

-.004

-.004

.860

-.004

0.00

.002

0.000

0.000

1:1

5787

1465500:1

84583:1

2631>:1

-11650

-11650

1.049:1

-11650:1

0

580000:1

0

0

a

63

Page 78: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

In order to sample specific locations at a distance from the instrument in-

take, a remote sampling probe (Figure 19) developed and deserthed In a previous re-

port (11) was used and evaluated for The instrument. The response of the pph level

analyzer is shown in Figure 20 for 200 ppb )c1U with the 5 foot Teflon probe attached

to the Instrument inlet. The response Is the same magnitude as the instrument with-

out the probe-except a slightly longer time is required to achieve the steady-state

signal. This means that calibration of the iiistruett without the probe, will not

cause error in the field when sampling with a prehe. iiouevcr it is rocoruended to

calibrate with the probe In place since this wiii also ensure proper probe performance.

The activity of the ?l sensor for all the hydrazittes i.e., II, tI, and UDMU are

measured. Results are stuinrJd t.n Table XXITI . A knowledge of this activity Will

allow one to calibrate the Inst. rent for ci liter ii, MM, or UL)t1I and by introduct lea

of an appropriate scale fractirn u!tanIng an ;t:rate surenr for each of these

vapors. The ppb anal y zer t:heii cal brated for MN)i vi I be cal ibated for H b y tnt] ti-plying the observed D'flI readIng liv 1.06, .nd t!IiJ le calibrated for UI)MII by multI -

plying the observed 1011i readings b y 0.37. Tb..:s, Calibration factors are acciirat. re

± 10% at present and are ape It at.' .1 .;i t ho ii near tuo

of the I ast runca how, \:t.*,*,

long term drift and tempera tttre i:''ct P ri si I es thes an tvcs have it beet

pletely verified. ContInuia ci f .:t; havo heri adct takn to 1-- , ice the crossrI

bration fractioo Ia order to be 11 00- t.i cc' ru vu tt-h Ins tt - ri'itt .itcd allow e r':ra t

field measurements of all ti'"ttv;'5 wtic o a sL cal Ir.tLic..

Hy draz Ines (H, MC11H, WPI) t1 c'n.. he.tc tcie'.l iudt'rce .'x I dat

composition in air (12,13, l . . [5 . Recenti v, we have observed titit the toxi.' ev,. I

analyzer does not give Lite s.tr.e rcs 'ns. t.1;U a A t a ud in,s in tie sattp ii it

sys tern. independently NASA ( 1 6) h'd obs' • tr. 'sn t . In order N r I v

1.•.., 'S

• - ''•--?,

.'.;;:.' 1!i:

Page 79: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

To ANALYZER PROBE RECEPTAC

5 FT. PROB

5 Fr. EXTENDE SECTION (3 NE FOR 20 FT. PR (

PARTICULATE FILTER

FIGURE 19

REMOTE SAMPLING PROBE ASSEMBLY

F.S

.1 1 I.,. I • I-.

Page 80: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

AIR

I 11 1 240 pP

200

100

120

80

40

FIGURE 20 EFFECT OF REWTE SA?'LINC PR0E ON 1W. RESPONSE

10

8 6 I. 2

Ppu

AIR S F!''

;'L vu

I 40 ;ctNs

i 20

i

! I

Page 81: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE XXIII

THE PROTOTYPE TOXIC LEVEL ANALYZER RELATIVE RESPONSE RATIOS FOR H. )(H AND UM

GAS CONC. (PPM) SIGNAL 31A/PPM RATIO (GAS:MMH)*

MMH .250 16 1:1

H .254 17 0.94:1

UDIflI .250 6 2.7:1

* Ratio is defined to be the PPM of gas equivalent to the signal of 1 PPM of P1MB.

67

I I'

Page 82: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

that the diffrence in Air/N2 reading is due to a sampling decomposition problem

rather than an artifact due to the ci :trochenicoi sensing i1pproa t,1 1 , the following 0x' perimer e s were undertaken. In one set of experiments, the fl1 permeation device is

allowed to equilibrate in air overnight, the PU4H/Air mixture is then introduced into

the electrochemical sensor directly from the permeation system. The experiment was

then repeated with N2 as the diluent gas. For comparison, colorimetric determina-

tion of the PQ*1 concentration is alno recorded. Results for this set of experiments

are summarized in Table XXIV.

It can be seen that both colorimetric and electrochemical measurements rive

significantly lower MMH concentrations In air than In N2. The lar;e c:) ncentrntion

difference observed In air can he attributed to the fact that a high temperature for

the permeation device (60°C) , long equilibration time with air and low concentration

of ?*ffl used all, maximized the decomposition process. To further support i:ii s by-

pothesis, another experiment was performed where the IM121 stre.un in N2 from the out-

let of the permeation system was mixed with either air (20 oxygen) or N 2 through

a Teflon T-joint before it entered the elecrrochemicl sensor. At all. concentrations

studied, no difference was c'bucrved for the M?tii concentration readout In air or in

Nitrogen (Table XXV and Figure 21). These experiments clearly support the idc'as

that:

1) Significant oxidolJ.ve decomposition had occured In t the permeation device

at the experimental cndttiuns 11 air was used as th di mont ;as

2) Colorlmet nc. me thds for du bc ticm of iIMH lack s p ec ii ci ty and a nt en': ra I

not sensitive to concentrations .25 ppm.

3) The electrochern i.ca 1 fn;ur is e loct lye rowa rd; and MNil, whe thur

in N 2 or Air s and nut. Ib., al. cim'osi tim mtL;

i(J?•'.• . os"

6 8

Page 83: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

OF' (.)j IG IYA L I ; i IS POoj

TABLE XXIV

COMPARISON OF ELECTROCHEMICAL AND COLORIMETRIC METHOD FOR THE DETERMINATION OF HYDRAZINES IN AIR AND IN NITROGEN

CONC. (PPM MMH)CONC. ANALYZED LCD READOUT

COLORIMETRIC ELECTROCHEMICAL

.288 (AIR) .0575 .O2S

.288 (N2) .288 .288

SIGNAL SIGNAL MMH (AIR) *!H 02 ) 0.2:1 0.08:1

69

.. .. . . . -,

Page 84: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE XXV

CO1rARS0 OF Tli E. FROTC)"'i"P E TOXIC LEV1!. !.X TO RH I.IN A I R

LD I\XI CONC. Wal (PPM) (PPM 1!) (FROM ?E1EATJ.0)

t. AIR

.309

•447 ./(8 .464

.577 .3

.665 .(O

Permeation f1wrtte: 2.

Air N,, fic..-rale: ì

-

Page 85: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

0

C

0

z

0

1.4 th

-

-4

z>

N

i .f.

x

x

,.-4

z

Page 86: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

A) Reliable caltbratian of zhe r5'tv' shu1 br

hydrti/in nttroen mixtures

(\JNt'LSWNS AND aCcNtVUCS

A prototype e1rcni thH't biq "s I e vol ''r

sensing e' been evc1o<t, ed f.tt'J md .

• supporting technoiv IiA4 th •c' cr '

COlI8 of a 5 feet. '1i T -''

carder and the prtot'' lovel rrt •'

surnt oi I, • 1-1 )-? ;'r I !

that thd 1nstruint is . t' t}e t- 3 r ft'rencs from t' sr-

tegut • r'i furliter ' • v c

requiru design ' \\\i. '.- 'S

The '-

method 11r \ •

dilkli-Ir i n

- .•S' S

t'rtn 'i ths& 7•.

.° •

S•5- • SS •

SS.. •,

.S- .

.. : • . - S * -

•5.1'

tht t-tt S-

••• S' ' •- .,'

•.:-

;P\'. s oit

Page 87: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I - •- - -.'S.

I--C I-

I Dli. i • - !- •èA'5.. - S

I. • • .._SI_p.S. •

Ak

-.- 1 11 '.• .1 -d S•

...S_• •p--.•S S • ••• •

_-

- .:.

Rti • • . . -- - 1 ILJL.)R

Page 88: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

TABLE ZIVI'

DESIGN GOALS

PORTABLE HPFUC0UC VAlOR DETECTION SENSORS

SPECIFICATION

Portable, Single Readout of

Hydrartnee Vapor Conc. in Air.

Senor responds to all Hydra-

-Joe types (H P01 and UDMI4). but need not differentiate

between then.

Accomplished

ACcOt2pl ished The unit is cali-

brated for the particular hydra-t ine of interest,

1NST1T TYPE:

SPEC IPICIT?:

PNGE:

SENSITIVITY.

TDQ'ERATU1E RANCE:

RELATIVE HUMIDITY:

DIMENSIONS (Maximum):

EIGHT

CAWSTRUCTION:

POWER-

Accomplished

AoopliShed

Accomplished

Acc.lished

Acco?p1ished x 3.94

Avccnp1i5bCd lbs. 4 o.

ratl. rhle I%i sunlight 3 digi t res1tt*.Also pro- I Accomplished

n rerth'r ottput.

rd proofed,

t tro t fl' it Accomplished

• trs Cflt inut'uS,

tth r,'vtst"' f'r lQ- I5V AC \'.'rrpl ish'.I

rjrth.U,Z'jack.

AL4:.UI'I' . light

t'r oVt'i . .\.' rpl I;h.i

0-2 prm with t P!B resolution.

0.05 rpM minimum detectable conc. readable to i 1 PPB.

o-oc

l(-.QS.

& SI' x 16"

12 ibs.

Page 89: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I S

'A UVII

INSTRUT PMUVXWAM GOALS

RESPONSE TIU (to 902 of reading chane at 0-1 PP or above)-.-

ACCURACY (at 0.1 PPM or above):

PRECISION:

URO DRIFT:

SPAN DRIFT:

NOISE:

TERFERENCES:

GAS

NH3

NO2

NO

SO,

0 Ar, He, cii ,l CO ,), FREON-12

H 2S

GOAl. SPECIFICATION

30 seconds minutes Virtually tdtata response to 25% signal and 4-7 minutes to 99-100Z eign1.

* lO

Accomplished (Dependent upon accuracy of cali-bration wathod and within precision of instrument.

112 P.S. Accomplished.

U P.S. per day Accomplished.

< 12 P.S. per day Accomplished.

± 12 P.S. per day Accomplished.

The following gases will give the interference ratio shown or greater:

RFERENCE RATIO COAL MINIM" TYPICAL

100:1 150:1 1,000:1

100:1 150:1 1,000:1

1,000:]. NOT DETECTED NOT DETECTED

1,000:1 3,000:1 5,000:1

5,000:1 NOT DETECTED

200:1 NOT DETECTED

500:1 NOT DETECTED

NO RESPONSE NOT DETECTED NOT DETECTED

1:1

I

75

Page 90: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

Present limitations of the sellaing technique r% 1fic[ty, resi tine,

sensor 1i1etje 1 and expanded detection ranges. Th cracterjsttc; an be in-

proved by further sensor developnents 1 and more fi.1d testtngs along !th improve-

ments in accuracy, en':tronnntul Stability, r.sJtivitv iind attttude iflsflltIvfty.

The permeation tube method of preparation of low conentratlon cf hydrtiinej

was evaluated and its reliabIlit y was 'tab1lshed IDY M-VA ri-14 011 with both o1ort-

metric and electrochemical methods. The Oic o':'ji rd Is f urther tblhthed

to be more selective than the color j trIc :uthd trds tH ecti. tIbrtI.

of the prototype toxic level atialy zec ir, t hus rkJ. to he dr '1th hvdrazine mixtures In nitrogen, a g Vx1d3ttv ctecoço.lti. 3 r oC -v.rLne hAs been shotni t o uccur In th prce.nce of air. The prototype .tnstr .'t t1- sL ro (frnc .: i;

spoa to coerc1aj h ydranes or air foc rad .ant :i dr:inpa.

applicatiorq of e1ectro:hanjcj s e nsing tc riO' i &' rde

of analy tical in g trucientaticn, d iwrer '' r ::prg'i!vn

1 :')L'

Page 91: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

REFERENCES

1. Thr . hoId Limit V83ut for Chemical Substances in Workroom Air, Adapted by

ACGIH for 1977. American Conference of Governmental Industrial Hygt'nt!;ts.

Cincinnati, Ohio.

2. K.C. Back, V.L. Crr and A.A. Thomas, Aviat. Space Environ. Med., .

591. (1976).

3. Standard T03t Methcd for Nitrogen Dioxide Content of the Atmosphere

(Grieas-Sa1n Reaction), D 1607-76, Annual Book of ASTh Standards,

American Soelty for Testing and Materials, Philadelphia, Pennsylvania.

4. NIOSLi Analytil i.thoda for Set Q, Report No. NIOSH-ScP-g. National In-

sttut for Oup:ticna1 Safety and Health, Cincinnati, Ohio 1976.

5. IJI. Kr'lzhc'.f C 3. kt Chem. Soc., 46, 2009. (1924).

6. H.E. M.iont: and R.A. 3tgers, Anal. Chem., 36, 1037, (1964).

7. J.A. J. hromatog. Sci., 8, 420, (1970).

8. L.A. D'. AI. ':m-., 43 9 1416, (1971).

9. a.:. Vt a. 'I Report, USAF/AFSC Contract F 41609-76-C-0029, Jun,'

10. J.R. stetre, 'S.uiv for Hypergolic Vapor Sens...r Development", Final pct.

Cutri f\-S 10-8982, April 8, 1977.

St.'tter 111 ti R.A. Tcllefsen, "A Study for Hypergolic Vapor S:

onI. Ftu.ii Thrt, NASA Contract NAS 10-8982, November 1977.

12. E.i. \'rn.' !.. LD. cEen, D.L. Geiger and C.C. Haun, "The Air Ox1,ie o

echyl:a'. Amer. Indust. Hyg. Assoc. J. 9 2. . 343. (I'

13. R.A. Sunkr od J.- Larkins. "Detection and Monitoring of Hydra.".

lh.-J t and Their Decomposition Products", Final Rep' .

Mc.oraidtu 'p.: 13, U.S. Navy , Naval Research Laboratory, Chen v

Dlvi iin, 'hvs I ci I Chemistry Branch, 23 pp. (1976).

77

Page 92: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

REFRCNCES (Continued)

14. P. Rartignoni, W.A. Duncan. J.'.. Murfreo. H.A. NappL . r, J. PI1iU.

and W.W. Wharton, "The Thrtl and "atalytIc of ?trhJ.hydrzines",

Springfield. Virginia, U.S. Dpartnvr.t of Cenz'rc, National Tcn1ci] Infotma-

tion Service, SI pp.. (NTtS J 764, 365), (1973).

1. Herb*rt McKenniR, Jr.,AndAllan S. Vir.i, "De rir1uc.'n of icc' rhv ihvdrztnc",

Anal. Chem., 26, 1960, (1.9.

16. R. Young. NASA, Ktedy Spr. 't' rer, Fler.l da, Cnmiu, i c t

I

Page 93: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

APPENDIX I OPBMTIOII OF PERMEATION TUBE CALIBRATION SYSTEM

A permeation tube calibration system is necessary for continuous generation of hydrasines vapor miaturee between 0.010 PPM and 5.000 PPM. The proparation of accurate and prsciae low concentration vapor blends using sealed percasetion tubes rG4Uir(s accurate control of the absolute toaperature of the permeation tube, procie control and accurate meaauromen of the diluent flourate and careful selection of aatrtala in contact with the low concentration blend. Figure 1 is a flowacheatic of a Modal 670 Kin-Tek Precision Calibration Syotem uaod for this purpose.

The system operates by maintaining a constant temperature at which a permea-tion tube anitte a known weight of the vapor at At constant rate into a diluent

stream of 99.9998X N2 . N2 was most frequently used as the diluent ainca hydrasines vapore were found to be more stable in N2 than Air. A controlled flow of the di-luent gas passes through a preheating chamber which is used to warm the gas to the same temperature at which the tube is thernostatted. It then passes through the permeation tube glaze chamber where it picks us and mixes with the vapor. The blended vapor then exits the system and is connected directly to the analyzer via a manifold which allow, venting of excess calibration gas through a scrubber - See Figure 2.

To set up the calibration system, the diluent gas source at 25 p4i (in the case of N2, a gas tank) is connected to the intake of the calibration system marked Diluent In and the flow is set to a point where the float of the .1 to 5 liter/ran. flovmster is raised just above zero. The temperature of the system to set to 60°C and allowd to warm-up for 1 hour. A 10 cm. H, P0*1, or UDP0I permeation tube which has been certified at 60°C is inserted into the system and allowed to equilibrate overnight.

The diluent flowrate Ia then adjusted to some rate equal to or greater than 2.0 liter/min. and the vapor mixture is ready to be sampled.

The concentration of the va..e can he determined by knowing the emission rate of the tube at 60°C and the Ilowrate of the diluent. The equation giving the ppm vapor concentration by volume is: .

CPxK 10' ppm

C - concentration of vapor leaving the system in PPM (volume).

P - emission rate of permeation tube in gram/minute.

K • unit cc-'version factor peculiar to the particular permeant vapor (24.45/mol Vt. of permeant).

F - diluel4t flourate measured in liter/minute at 25°C and I atm.

(For example using 10 cm. tfH tube at 60°C whose certified rate - 1,086 ng/min.

and N 2 diluent flowrate of 2.5 liters/minute.

Pt1H] - 1086 x l0 j m./mtn.x0.531 liters/gm. 6 x 10 ppm 2.5 liters/min.

- 0.231 ppm

Concentration can be changed 1w altering flourate, varying temperature, or using

varied quantities and/or lengths ot permeation tubes.

79

Page 94: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

0 -J

I I

I •1'

DILUENT IN

FLOW CONTrUt.

PEflMEAT ! ON

--.-

CALIBRATION

GAS OUT

I N ST RU ME N I FRONT PANEL

F

F CiW rL!:\T L

K I TE': ;:) (.: I I I:

Page 95: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

SU

VFNT

CALIBRATION (AS

FIGURE 2

SYSTEM FOR CALIBRATING HYDRAZNES ANALYZER

31

•\\

Page 96: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I

APPENDIX 11

OPERATION OF TILE IjYDRAZLNES DILU11014 .\PPMATUS

A. The Hydrazine Dilution AppartuI is used to mnk hydrazics vapor mixtures,of r

1. ppm to ) 100 ppm in a continuo nnnn'r. The dil ut i.'n appriltus Is shown in

FIGURE I-A-i, which is contai.ned 1t a I.irgc fume hood, sthce the hydrRineS are of

toxic and dangerous aeture. Mu, any botti's or vials of neat hvraznt.s are kept

in the hood.

The apparlitus operbtes by supptvag a oat (aria 3ow f I co cf Itqtdd HydrazItic.

H, or UB1H conta!wd in a 10 it'. !4arnItnn syringe with a 5a' Model 35 syringe punp

through septum eaii part I nto a custom f;ahrit:tcd glaca mixing apparJn Llirotui.h

diluent gas fIote. 99-999t11' N 2 most f ri'quoflt ly ued a 6.1u . nt t nCc.

hydtazthes vapers were found t. he ñur.e stable in fo.i then air. A ca r1Id flow of

the diluent g3s passer through a pre-condtttoalng chather, which may he i:sed to warm

the gas stream wheit it' lit 1vt lv I I ii t'ici'nt r.i I :i;') 'i 'Jr:iint'art iesir-.

ed. It then pase8 tIti' 'Y t J ne need .' I ek nj up h' vapor and ta to i I I tec bu '

whdi mixes the vapor and dl lueitt gas. The vat ' i' r"'i xi tre then atv be d ivd by wi'

tef.on glass valv•s ,u(l Ill.- namp Lin. (it !1tt.)iC:si.3tt fi,.tnet.er. The

p . r r n;I.xtttrei r'av 0 Lilt r ho re I c'.t.d in Ici I, . ter rena nt or be uied

f ..irn the s!P.Ie .'(L'...........

To set up Cie d; 't ill 1'.et S\.,t'"i. a, 1 lieu' • ,e' t.,'.I_ flt .i .I1 )S(2 01

a gas tank) s :or'nt' tel 1.' :r..ini,i1.1 ..... ti i ueI Ni tin' F.

nil x ne, ap p a i- a tilS. ft C' it I 'n-i, i. .,1 .' d e' '.1 t...I' cc 4 _ n r.; sam-

a) eIi OW(&' tCt Wi t_ti I......a'. I ''e.. ii) tv.ti.. '. at .., .' u I ul' ffl;f

fold. A In avrin.c ijiie. t.i. iou,,d,.i.:. 'i 1I:P! t,ci:i :i Ti'f•a; v:iI:e

i , p •J ()tiar.l :i.' ;.r'p..'l :':a.. ' ' .. .t ............, .'. •.,u ",Ic(it,ti I itt's Ifl

''a1 rfanvt' hubh - , .. . . 1 I, ii the Cp' ui-i

I titthu 'lass i-il 'I. lie . . ..j 'n

t lai:tp. The svr I iige atu1jI

/ .i:.. . •c : ?...::1:-' 1:

Page 97: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

put on a high speed until the carriage is just pushing the syringe plunger. The pump

1 to then adjusted ,.o some lower delivery rate (for example settings 60% flow X 1000).

After allowing 15 minutes for the system to reach steady state, the vapor mixture is

ready to be sampled.

The theoretical concentration of the vapor can be found by knowing the delivery

rate of the liquid and the flourate of the diluent.. The equation giving the ppm vapor

concentration by volume is: ml AD X 24450 mole X 106 ppm

EMNII, H, or UDMHJ • MF

ml where: A • the delivery rate Hydrazines liquid ( mm ).

D • the density of the liquid (g/ml). ORIGINAL PAGE IS Pooi:"

H - the molecular weignt of the liquid (mole).

F - the flovrate of the diluent (all mm).

Since the syringe pump delivery 0.024 ml/min for a 10 iii syringe at pump setting 100%

Flow X 1, A is given by:

BC(2)

A - 0.024 ml. mm 1007.

• where B 7. Flow

1 1 1 C=Xl, Xj, X3j orXj

Substituting equation (2) into (1) gives: 0.024 ml/min BCD X 24450 nil/mole C 106 PPM

[MV, H, or UDMII) = H F 100% (3)

('or txample MP at pump settings 60% X and diluent flow of 700 ml/min yields

0.024 al/mm x 0.866 guI x 60% x I x 24, 450 ml/mole x 106 ppm [NMH]= 1000 9.4ppm

x 46 g/mole x 100?. x 700 ml/mm

Bag samples are collected by disconnecting the sample stream from the flownieter

and connecting a Teflon bag to the sample stream. The ag is left on until it is 95%

full. The bag Is then removed and its valve is closed. The sample stream is replaced

on the fiowneter. The bag may tncn be calibrated colorim'itrlcally or electro.iemi(a11y

..,.., and used for remote sampling.

U

83

Page 98: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

For direct sampling the sample stream is connected to a 500 ml plastic bottle

with a sample exit and a vont. A portion of the sampl.e stream is then drawn for

testing.

!'•:--- r. - .-

Page 99: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I-4

IiV OP THE

13 POOR

4 1.1 a

U .-J* OI.s-4

.

mom !!i i

4

T Sa

to in

IC4 Id [7

46 Vol 49

Page 100: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

APPENDIX Ill-A

DETERMINATION OF GASEOUS MONOMETHYLHYDRAZINE

A. Preparation of POMAB Dye Solution

1) MIX:1.6 S. dimethylaminobenzaldehyde

15 ml concentrated MCi

200 ml Methanol

2) Store the dye solution in an amber bottle in a dark place.

Shelf iirz two weeks.

B. **I Stock So1uiofl 1 100 ppm

1) Carefully weigh 0.156 g. of MMII. H2SO4 salt on an analytical balance.

2) Completely transfer the MMM . H2SO4 to a 500 ml volumetric flask con-

taining about 100 ml. 0.1 N H2SO4. Shake the flask, dissolving the M'W.

H 2SO 4 . Fill to the mark with 0.1 N M2SO4.

C. Use of the SpectroniC 20 Colorimeter

1)With the instrument off, ensure that the "blue" phototube, number

CE-A59RX (gray internals), for wavelengths less then 650 mm is installed.

2)Turn the instrument on by rotating the Power - Zero control clockwise

and allow the instrument to warm up at least 30 minutes before use.

D. Samp ling,

1) Pipet 25 ml of 0.IN H2SO4 into a midget impinger with a bubbler attachment.

2)Connect the Inlet of the impinger to a female fitting to allow easy bag

sampling. Connect the outlet to a flowmeter and the flowmeter to a valve

and the valve to a pump with tygon tubing (See Figure

3)Turn the pump on and adjust the flowratc between 700 and 200

cc/min with

the valve. NOTE the flowrate.

4)Cal :ulate the time needed to collect the desired volume of OI/N, or flu/Air

by the equation:Volume_

Collection time (Minutes) F.R. (cc/mm).

Connect the bag sample or other source of fl1 vapor to the impinger inlet

and start stopwatch.

5)After collecting for the desired time, remove bag or other source of 1*Ui,

stop stopwatch and turn off pump.

6)Collect 106 liters at 0.1 ppm MM1, 10.6 liters at 1 ppm ?OIH, and 1.06 liters

at 10 ppm 1H. This volume needs to be determined by trial and error for

unknown vapor samples.

Page 101: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

,-

. S

S. Anelveis

1) Turn on the Spectronic 20 and allow it to warm up.

2) Prepare a blank by pipeting 5-ml of 0.1N H2SO4 to one of the teat tube

cells supplies with the coloricieter.

3) Pipet S ml of the aample solution In the imptngev to a colorimeter teat

tube.

4) Pipet 2 ml of the PDMA3 dye solution to each of the teat tubes.

5) Stop per the teat tubes and allow to stand for 30 minutes.

6) After 30 minutes, read the Zr as

a) Set the Spectronic 20 wavelength dial, at 457 am and

adjust the zero control so th't the meter reads OZT

with the cell holder enpy and the cover cloned.

b) Ensure that there arc no huhble9 in the blank sample

and wipe the o '.tn1.de of the cell. clean with a tia8ue.

Open the cell holdc'r cover and insert the tent tube

cell, aligning th: ;nark on the cell with the line on

the holder.

c) Cloue the cover and adunt the LIGHT control until

the meter reads 100%T.

hoo d) Remove the blank and save for future use.

e) Ensure that the sample cell contains no bubbles and

wipe the outside clean with a tio'ue. insert the

cell in the holder, aligning the nark on the cell with

the mark on the holier.

f) Close the cover and rend T. 0TE the results.

g) Repeat, steps b,c,d.., and f thre '' times and take

average %T value.

7) Remove sample fron ccIorter. IfsampLeq have been pre-

pared for caeaurC2nt, re.cat. st (zo tirough lig for each sample.

8) Convert the average T o f the sample :o A (absorhonce) b y the formula:

100

A - ic (ZF )

9) Obtain the fl'.}'. value Iron the caUbttJon cur'.'.

' TM

13JOl ORIGINC

Page 102: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

F. Calculation

The concentration of gaseous HHH in N2 or air is found by the equation:

V

A • ppm 140 in the solution sample.

V • volume M)OI/N2 or HM/Air collected in cc?

C. Calibration Curve

1) Prepare a 10 ppm )*I standard solution by pipoting 10 ml of the stock solution to a 100 al volumetric flask and diluting to the mark with 0.111 R2SO4 . Repeat for standard solutions of 8,5,2 and 1 ppm )HR by pipeting 8,52, and 1 ml respectively instead of 10 ml.

2) Follow steps El through E8 in the analysis using the standard solutions as samples. Plot A, abeorbance, vs. ppm MM on graph paper. Draw the beet straight line through the points and extrapolate to 0 ppm.

3) A separate curve shall be prepared for each colorimeter. A new curve, shall be prepared if it is necessary to change the colorimeter lamp or phototube.

4) Standard samples should be run periodically (i.e., one with each days calibrations) to check the accuracy of the calibration curve.

NOTE: This procedure may be modified to fit the in"ividual operators needs.

Page 103: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

I

I I -

S

S

• •.

S

.4.

S

• .•

4

: jL'y 01 S

GE IS PO(Y.

S S

I

Page 104: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

- - - - -. -

U

APPENDIX 111-8

DETERMINATION OF GASEOUS HYDRAZINE

Preparation of PDMAB Dye Solution

1) Refer to Section A in the Determination of Monomethylbydrazifle

Appendix It-A.

NHi Stock Solution, 100 ppm

1) Carefully weigh 0.152 g. of N2H4.(HC1)2 salt on an analytical balance.

2) Completely transfer the N2H4.(HC1)2 to a 500 ml volumetric f!tak containing about 100 ml O.].N RC12. Shake the flask, dissolving the

N2H4.(HC1)2. Fill to the mark with O.1N Nd.

C. Use of the Spectronic 20 Colorimeter

1) Refer to. Section C in the Determination of MonomethyihydraZifle;

Appendix 11-A.

D. Sampling

1) P ipet 25 ml of 0.1N HC1 into a midget imnpinger with a bubbler attachment.

2) Refer to Sections D 2-5 in the Determination of MonomethyihydraZthe,

Appendix It-A.

3) As a guide, collect 19 liters at 0.1 ppm II, 1.9 liters at 1 ppm H. and

0.2 liters at 10 ppm H.

E. Analysis

1) Turn on the Spectronic 20 and allow it to warm up.

2) Prepare a blank by pipeting 25 ml of 0.1N HC1 into a small vial.

3) Transfer the entire impinger sample to a small vial.

4) Pipet 1.25 ml of the PDMAB dye solution to each of the vials.

5) Cap the vials and allow to stand for 20 minutes.

6) After 20 minutes, read the Zi as follows:

a) Set the Spectronic 20 wavelength dial at 457 on and adjust the zero control so that the meter reads OZT with the ccli holder empty and the cover closed.

b) Rinse a test tube cell twice wit.i the blank and fill halfway with the blank. Wipe the outside of the cell clean with a tissue. Open the cell holder co y:: and

insert the test tube cell, aligning the mark on the cell with the line on the holder.

4

1.

11

Page 105: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

C) Close the cover :*4 a d just tt,: LIGHT control until the mater rt'. lOOT.

d) Raz.ive the Lank td save for future use.

e) Rinse a .r11 twice with the sample and fill halfway with the sample. Wipe the outside clean with tissue. Inser the cell in the holder, aligning the mark on the cell with the mark on the holder.

f) Close the cover and read %T. NOTE the re-suit.

g) Repeat, steps b,c,d,e, and f three times and take average %T value.

7) Remove sample from colorimeter. If additional samples have been prepared for measurement, repeat steps 6b through 6g for each sample.

8) Convert the average ZT of the sample to A (absorbance) by the formula:

A log ( 100 )

9) Obtain the N2H4 value from the calibration curve.

F. Calculation

The concentration of gaseous N2H4 in N 2 or air is found by the equation:

ppmN2H4A 19.1 V

A - ppm N 2H4 in the solution sample.

V - volume N2114/N2 or N 2114/Air collected in cc?

C. Calibration Curve

1) Prepare a 10 ppm. N2 114 standard solution by pipeting 10 ml of the stock solution to a 100 ml vclumetric flask and diluting to the mark with O.1S HC1. Repeat for standard solutions of 8,5,2, and 1 ppm N 2H4 by pipeting 8.5,2, and 1 ml respectivel y instead of 10 ml.

2) Follow steps El through E8 in the analysis using the standard solutions as samples. Plot A, absorbance, vs. ppm N21-1 4 on graph paper. Draw the best straight line through the points and extrapolate to 0 ppm.

3) A separate cover shall be prepared for each colorimeter. A new curvi, shall be prepared it if is necessary to change the colorimeter lamp or phototube.

4) Check calibration often by analyzing a standard sample.

C.-,

Page 106: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

n

APPENDIX Ill-C

DETERMINATION OF GASEOUS UNSYMMETRICAL DIMETHYLHYDRAZINE

A. Preparation of Buffer Solution

1) MIX: 9.6 g Citric Acid 15.7 g NO2HPO4 2 liters distilled water.

2) Adjust the pH to 5.4 (with a pH meter)? with citric acid?

B. UDMM Stock Solution

1) Fill a 500 ml volumetric flask with buffer solution to the line.

2) Transfer (63 x (purity of UD) ) iiL of neat UD?ffl with a 100 uZ syringe

to the flask. Shake the flask.

C. Use of the Spectronic 20 Colorimeter

1) Refer to Section C in the Determination of Monomethylhydrazine Appendix

II-A.

D. Samp1ing

1) Pipet 25 ml of buffer solution into a midget impinger with a bubbler attachment.

2) Refer to Sections D 2-5 in the Determination of Monomethylhydrazine, Appendix Il-A, however the flowrate through the impinger should be between 200 and 400 cc/mm.

3) As a guide, collect 33 liters at 0.1 ppm UDMH, 33 liters at 1.0 ppm UDMH, and 0.33 liters at 10 ppm UDMH.

E. Analysis

1) Turn on the Spectronic 20 and allow it to warm up.

2) Prepare a 0.17. TPF solution by transfering 0.1 g of trisodiurnpenta-cyanoaminoferrate into 10 ml volumetric flask and filling to the mark with distilled water.

3) Prepare a blank by pipeting 7 ml of the buffer solution to one of the test tube cells supplied with the colorimeter.

4) Pipet 7 ml of the sample solution in the impinger to a colorimeter test tube.

5) Pipet 1 ml of the TPF solution to each of the test tubes.

6) Stop the test tubes and allow to stand for 20 minutes.

7) After 30 minutes, read the %T as follows:

93

Page 107: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

a) Set the Spectronic 20 wavelength dial at 500 nm and

adjust the zero control so that the meter reads OT

with the cell holder empty and the cover closed.

b) Ensure that there are no bubbles in the blank sample

and wipe the outside of the cell clean with a tissue.

Open the cell holder cover and insert the teat tube

cell, aligning the mark on the cell with tre line on

the holder.

c) Close the cover and adjust the LIGHT control until the

meter reads 100XT.

d) Remove the blana and save for future use.

e) Ensure that the sample cell contains no bubbles and

wipe the outside clean with a tissue. Insert the

cell in the holder, aligning the mark on the cell

with the mark on the holder.

f) Close the cover and read %T. NOTE the results.

g) Repeat, steps b,c,d,e, and f three times and take

average %T value.

8) Remove sample from colorimeter. If additional samples have b .n prepared

for measurement, repeat steps ôb through &g for each sample.

9) Convert the average %T of the sample to A (absorbance) by the formula:

A log (.1P_)

10) Obtain the UDMH value from the calibration cur-.-c.

11) NOTE: UD!11 impinger sample should be analyzed within an hour of collection.

Calculation

The concentration of gaseous IJDMH in N 2 or air is found by the equation:

9.55 ppmUDilA V

A ppm UI)MH in the solution srplo.

V volume UD'ffi/2 or UD/Air collected in cc

F

• L

OM

Page 108: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

Calibration Curve

'.) Prepare a 10 ppm standard solution by pipating 10 ml of the stock solution

to a 100 ml volumetric flask and diluting to the mark with 0.1N H2SO4. Re:eat for standard colutions of 8,5,2 and 1 ppm tI by pipeting 8,5,2, and 1 ml x respectively instead of 10 ml.

2) Follow steps El through E8 in the analysis using the standard solutions 68 samples. Plot A, absorbance, vs. ppm !fl{ on graph paper. Draw a curve through the points and extrapolate to 0 ppm.

3) A separate curve shall be prepared for each colorimeter. A new curve, should

be prepared if it is necessary to change the colorimeter lamp or phototube.

95

Page 109: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

Diaving CSt-852 is the electronic circuitry that describes the prototype

1^,

toxi' level atalyzer'8 electronic components and deaisn..., '1

The following sections describe the function for ecch.of the components

in the circuitry. I. .

Ok' 'E1-jj ORTGThAL PAQj IS POOR

F

9t;

11

/

Page 110: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

£1

4 1 Ali f I

Ja

JGS

IL

•1

ALft

(.) e SW i' (!) IPA A(b'

, !.—.-<(.. •q•

±81 •®TiT 01

c.l• —0

A' ••11 ,!_; acc 'I

- £4

--.--' ---------

BATTERIES AND BATTERY CHARGER CIRCUITRY (T ()

VOLTAGE REGULATORijp..,.

r1 a..,, L{

C

CAI

051 —r a1

REPROr\UCIBIL ITY OF THE ORIGINAL PAGE Is POOR

-4r

V $.•,

EV

/

Page 111: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

- 02)jOLD.OLT. I:lAIE

, cearoI 9,.

%l#4 6.4-- —.

—A/---- 4Jc'%

aa.içG •

'so

vu OS7

'4,

j,( r r

ir LXj}'

AD

cao

L4 vi

••

Id1 ICE - CA314OAT IC? - LM32tb 1C8 - D14011AE

1C9 IC1O - I14317I h. 86 - GE TYPE D Ni/Co

AUDIBLE A

oz

a,

us

LOW BATTERY CIRCUIT

v_

4 tc#4

,. ,I 4

1 et_,

lop

C

,_,,, if 7 7X,2

PAN CONlitOL

' 1 A "u ()

L.-46 c'cj itt

ITRY]j .4T1 ,':; 1iC ____

-I 9

J'7 V

(r)

R55 • VISUAL ALARM

VAJ

1—Ago 3AI 1.

CORDER OUTPUTI

sws

._ e

ILLLJ1INAT.I$

lda POWERON/OFF • I

V.4.. (S'

ST

.uuu G tl.iwftIEpERGEflc5 SCIENCE INC. IV3LS £413 CaII

LNSFORD. N.Y.— PC?1S * 'I4

s*clr*II I P1. * 11 SCHEMATIC 0 - 2 PPM 'Pft.* o" I Its- HYDRAZINES ANALYZER

ALL IlIli ALL

-.--- .1k LTI ICAL i'mi' •

I C1. 1',,'.n,.

.1*. II.

ccce,57 ______

I..'

Page 112: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

APPENDIX IV

ELECTRONIC CIRCUIT DESCRIPTION

Potential Circuit

The potentiostat's function is to maintain a constant potential difference

(Er,) between the working and reference electrodes of the sensor. Operational

amplifier IC-1 performo this task. The potential Erw between the reference and

working electrode is kept exactly equal, the voltage at the positive input (pin 3)

of IC-1. Variations in the resistance of the electrolyte have no effect on Erv.

Moreover any change in the electrochemical potential of the counter electrode is

also compensated.

When gas is oxidized at the working electrode, the potentiotat provides

th power to sustain the reaction. The output of IC-1 (pin 6) will swing nega-

tj a and the necessary current goes through R3 to the sensor. This current,

viii. t is proportional to the gas cor.centration, causes a voltage drop across R3.

This voltage drop is applied to the differential amplifier.

Differential Amplifier

IC-2, IC-3 and IC-4 constitute the differential amplifier. The use of three

Op Amps results in a "classic" instrumentation amplifier. This configuration re-

suits in high input impedance, low offset and drift, low nonlinearity, stable gain

and low effective output impedance. The gain of this section is 5.97. The output

of the differential amplifier (IC-4, pin 6) is applied to the temperature compet-

sation amplifying circuit.

Page 113: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

- - y-.'--'-r --..--,---,_ •---

-

Te^Verature Coeneation Circuit

This circuit is cortfi&ured as a summing amplifier with temperature dependent

gain. At 25°C the gain, in unity. To compensate for- variations in the electro-

chemical reaction rate of the sensor a thermistor (R4) is placed in the feedback

loop of IC-S. The sensor typically has a positive temperature coefficient while

the thermistor has a negative temperature coefficient. The feedback resistance

of 10-5 (R4, R23, R27) is scaled to counteract the sensors characteristics

Since the gain is varied there is no dependence on gas concentration. Sho'ld

zero temperature compensation be required, provisions have been made to use

thermistor R65 and resistors R66 and R67. The background current of the sensor

mulled out by the zero control R20. However, the background current is tempera-

ture dependent resistor, current is added or subtracted from the summing junction

of IC-5 thereby compensating for variations in sensor background current with

temperature.

Voltage Reference Circuit -

Various reference voltages are required throughout the instrument electronics.

Diodes Dl and 02 provide the basis for the reference voltages. They are tempera-

ture compensated, low, voltage reference diodes employing a band gas technique to

insure stability. The nominal voltage of these devices is 120 V.

Zero Control

The zero adjust potentiometer (R20) is connected to the ± 1.20 reference

voltages. The center tap voltage permits current to pass through R21 and into the

summing junction of IC-S. This technique allows the instrument to be zeroed.

Page 114: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

----

.0

Span Control

The output of the temperature compensation circuit (C-5, pin 6) is applied

to the span control potentiometer (R28). Amplifier IC-6 is a voltage follower

with gain. In this case the gain in 6.6. Potentiometer R53 is used as a zero

offset adjust. In practice, the span control potentiometer is rotated counter-

clockwise so that the center tap is at ground potential. R53 is now adjusted

until the LCD display reads .000. Capacitor C30 is used to ptevent IC-6 from

oscillating.. The output of this circuit is applied to various circuits through

resistor R42. These circuits include the LCD display, alarm comparitor and

recorder output.

Alarm Circuitry

1C7-A is used as a voltage follower with variable gain. The 1.20V reference

voltage is applied to the non-inverting input of 1C7-A. In practice, R29 is ad-

justed so that the output of 1C7-A (pin 1) roads 2.00V. This 2.00V signal is

applied to the alarm set control (R3). Since 2.00V represents the full scale of

the instrument, rotating the alarm set control will provide comparitor 1C7-C with

an input ranging between zero and 100% full scale. The other input to 1C7-C is

the analog signal representing the parts per million of the gas being detected.

As long as the analog signal input is less than the alarm set voltage, the output

of 1C7-C will remain low. When the analog voltage input exceeds the alarm set

voltage, the output of 1C7-C will be switched high.

Visual Alarm

When the output of comparitor Id-C goes high. NAND gate 1C8-D also goes

high providing current to the base of Q2. Transistors Q2 and Q3 are arranged in

a Darlington configuration to provide sufficient current to illuminate the CE44

lamp. This lamp will remain illuminated until the analog signal falls below the

alarm set level.

Page 115: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

Mr --- 'jr- - Vfl

S -

Audible Alarm -

When the output of comparitor Id-C goes high the audible alarm is activated - -

through the Born ON/OFF switch (SW-3). Transistor Ql is used Lo ensure that sufficient

current is available to drive the audible alarm. The audible alarm will be silenced

If the analog signal falls below the alarm set level or if the Horn ON/OFF switch

(SW-3) is placed in the OFF position. - -

LCD DiSplay - -

The LCD display 13 a modified DATEL Model 310OX digital panel meter. It has

a full scale reading of 1.999. In positive over-range the display ready 1. with

the remainder of the display blank. In negative over-range the display shows -1.

with the remainder of the display blank. Positive over-range occurs when the analog

voltage input exceeds 1.999V. Negative over-range occurs when the analog voltages

is less than -1.999V. The DATEL 3100X is modified by the addition of two lamps

(GE-1784) to provide illumination in low light environments. Putting the-display .1 -

illumination switch SW-5 in the ON position will turn on these lamps to provide

viewing in dark areas. Lamp life is rated at 1000 hrs. -

Recorder Output - - -

The recorder output provides both analog signal and power to run a portable

recorder. The analog signal is O-IV representing 2 ppm. The recorder output cir-

cuit is designed to utilize the 1000 ohm recorder impedance. When connected to the

F.COLYZER, the recorder impedance is in parallel with R60. This parallel combination

is in series with R59 and together act as a voltage divider, halving the 2V full

scale signal of the instrument.

NOTE: If a high input impedance voltmeter is used, a 1000 ohm, I resistor

must be placed across its input.

-F

Page 116: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

-- -••

Power ON/OPT

In order to easure minimum warm-up time, the sensor is always kept under po-

tentiostatic control. However, to miaimire battery drain, power to the remainder

of the Instrument is turned off. The power ON/OFF switch performs this, function.

The power ON/OFF switch also is used to turn on the pump.

Battery test switch SW4 samples both positive and negative battery supplies

and displays the sampled voltage on the LCD display. Resistors R61, R69 and R62

are used as voltage dropping resistors. The voltage drop across R69 is displayed

on the LCD meter. Any voltage above l.000V shows good batteries; any reading below

• 1.000V indicates that the batteries reçiire recharge. Readings below 1.000V will

occur when the Ni/Cd batteries reach an individual voltage of 1.22V.

• Low Batten Alarm Circuit

Id-B samples part of the battery voltage appearing across R36. The output of

S

10-B is the input to .comparttor 1C7-D. As long as this output is above 2V the

batteries do not require recharge. Below 2V the coinparitor output goes low turning

on an oscillator comprised of NAND gates 1C8-A and IC1-B. The oscillator frequency

is approximately MHz. Use of diode D3 causes the wave form to be asymmetric.

The ascillator output is applied to the base of Qi which energizes the audible alarm

in a series of "beeps".

NOTE: An alarm caused by a high gas concentration will override the low

battery circuit and the alar-a will sound continuously.

Function Test

The function test enables the user to check the instruments electronics except

'for the potentiostat circuit. By depressing function test switch SW2, a current is

fed across R3. The additional voltage drop is sensed by the differential amplifier

and is applied throughout the various circuits to the panel meter. This injected

voltage should cause audio and visual alarms to energize (depending on the positions

102

Page 117: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

of the Span control and Alarm Set control).

Batteries and Battery Charger Circuitry

The instrument is powered by six "D" size nickel cadmium rechargeable batteries

each having a capacity of 4 Ampere-hours. Charging is accomplished by connecting

the charger to the charging jack. Resistor R56 controls the charging current and

diode 1)4 prevents damage due to an accidental shorting of the charging jack. Charg-

ing time is overnight (16 hra).

Pump Voltage Regulator

This circuit employs a LM317M voltage regulator (IC-9) to provide a constant

voltage to the pump regardless of load. It will supply sufficient current for the

starting torque and will adjust for varying load conditions and battery voltage.

The voltage is regulated at 4.3V.

H

Page 118: A Reproduced Copy - NASA · k-CR Toxic level hypergOlic 33 vapor detection sensor development. A Reproduced Copy OF t Reproduced for NASA by the NASA Scientific and Technical Information

- • -'r-

- e-&•.• -• - --

'-•-

F - tW f4•__ •3;- - r -, \ •;-'-: J Ad

-r-

-J.L ----•- - .--'•---•- -.--.•---

- • -• • 4 - - - - - —

V.

Wrl

I ; } (\J -:- - -'- -- --- - - --

-_L - -- —-•---