toculator in temperature (pi925,") rose above -291 do? at 11.5 minutes and re-mined warmer than...

59
UNCLASSIFIED AD NUMBER AD834023 NEW LIMITATION CHANGE TO Approved for public release, distribution unlimited FROM Distribution authorized to U.S. Gov't. agencies and their contractors; Critical Technology; 19 AUG 1959. Other requests shall be referred to Space and Missile Systems Organization, Los Angeles AFB, CA. AUTHORITY SAMSO ltr, 10 Apr 1972 THIS PAGE IS UNCLASSIFIED

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Page 1: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

UNCLASSIFIED

AD NUMBER

AD834023

NEW LIMITATION CHANGE

TOApproved for public release, distributionunlimited

FROMDistribution authorized to U.S. Gov't.agencies and their contractors; CriticalTechnology; 19 AUG 1959. Other requestsshall be referred to Space and MissileSystems Organization, Los Angeles AFB, CA.

AUTHORITY

SAMSO ltr, 10 Apr 1972

THIS PAGE IS UNCLASSIFIED

Page 2: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

ct~

I

Page 3: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

-de&CONVAIR ASTRONAUTIC NCLASSI FlED-

fths document Is zab3"%

PWS TI tZP T 2DA eCa' * -

SPECIAL TS

Wn~ 4 9

LI13iKARYon ~ HSTh ENGINEERING S1JPPGT MIOUP (~

AIND\9 jTET, EVALUATION (ROUP

ISSMI s 19 A'UM~T :959

APPROVED BY V q

zngineer:Lig Su,: O-t o Z. 'a

Group Engineer tg Cjr3 4* *JO

Soy- A4~APFROVED B!

Senjo: LIigbt TestGroup Erviiier

APROVED BChief~ Test Condtiotor

Thi, document contains information affecting thoa IoA N eae ithin the meaning of the Espionag- Laws, Title 18,USG, Sections 793 and 794 The trnmssoW~ tJ44o, 00 s c ~ ED hrie person is priibited by low.

FORM NO A 702 2 4 1

Page 4: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

Addend=zM( 129

CONVAIR ASTRONAUTICS UNCjjASSIFEQj

SEURITY NOTICE

This document containi information affectingthe national dcfenae of the United Stateswithin the moaning of the espionage l~aws,Title 18, U. S. C. Ssctions 793 and 794. Thetransmission or the revelation of its contentsin any manner to an unauthorized person isprohibited by lav.

This document contains information affecting the' national defense of the lJnttd States within the meaning ofi the Isp-onage Laws Ti t !8USC Sections 793 and 794 The transmrission or toe revel jticin of its contents in any manner to in unauthorized person IS Droii,0utcd by A

wqm 1,0 A 702 2 A~nn~NCLASSIFIED

Page 5: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

41WOM WK dn&

CONVAIR ASTRONAUTICS ME iii

TABUE OF CCFTEIT

We. of

Senwiity Notice lTable of Contentsii1Section lt1: Sainry 12Section 2: Fuel loading System 3 1Section 3:1 I2 Loading System 42Section )a LX2/liu loading System 6 2.Sectio~n 5: Convafr Propellant Loading System 7 1Section 6: Lcoustica Propellant Loading System 8 1Section 7: Missile Tank Pressluriz.ation 5ysteur 9 1Section 8: Ground Support Equipwnt 10 1Section 9: Data 11 1

Time Slice 12 31. A. Data 20 12

Section 10, Instrumentation Survey 32 3Appendix 1: Tables and Figures 35 18Appendix 2: Operating Conditions 53 1

Red Values Exceeded 541Aope'-dix 3:t Test Article History 55 1

PRocedure History 56 1Appendix 4: Distribution 57 2

Total Pages 61

,,S diOCij-nt _OrtarrS nfo'md;-Gn affect ng tthe national deferst, of !he U toStates within the meaning of 'he Espioniage aws TItie 18,jKC Sec, OnS '3 and -,,14 Tse tar% eSSo'or the evelatjonof iscc' ents in any manne, lo an ursluthoilled pe'sor is piohibile iy law

~SWLAzI&

Page 6: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

AddendumWgTX1299

CONVAIR ASTRONAUTICS UNC[ASSIFIED PPAF

SECTION 1

Summa 2

VRuns 95-423, 424, 425, and 426-SP2-Sl were satisfactorily performed at TS

1-95 on 4, 5, and 6 August 1959. These runs fulfilled the requirements ofspecial test SP2. ( f_

The engine L02 tank fill times and discussion may be found in the originalSK 1299 report.

L02 and fuel were loaded at IOC rates on all four runs. The Acoustica PLCSproperly controlled the loading sequence during Runs 424 and 426. The fuel90% probe signalled RAPID LOAD STOP before the fuel rapid load valve openedduring Run 423. Fuel rapid loading wa3 continued manually. The L02 90%probe signalled RAPID LOAD STOP at approximately 68% L02 tank level duringrapid loading on Run 425, L02 rapid loading was continued manually. G02samples were taken during L02 tanking and detanking periods for determinat-onof G12 contamination during Runs 423, 424 and L25, but not during Run 426.

Booster helium bottle temperature and oressure requirements for 65-2 wereachieved during Ran 423. This was the fourth consecutive run on which 65.-2requirements have been achieved. HelLum load start was delayed 3 minutesafter FUEL LOAD START, as planned. The aerage temperature attained duringRun 423 at 13.0 minutes was -299 DGF *ith 3060 PSIG in the booster heliumbottles and with the LN2 high flow rate less than 86 GPM. The charact::Lsticdroop in booster bottle pressure was repeated during this run prior to LhePS-80 cutoff point, recovering to 3060 PSIG at 11.9 minutes. Helium loaaing

was not attempted during Run 424, but LN2 was loaded to simulate engine com-partment environment. Helium and .N2 loading were not attempted during Rw-o

425 and 426.

The L02 topping valve did not open during Run 423 due to rust in the valvepositioner, caused by condensation. The L02 Recirculator In temperature(P1925T) rose above -291 DGF at 11.5 minutes and remained above that tempera-ture until drain start. The L02 tonping valve remained full open (25 to 28GPM) during the L02 topping hold rn Runs 424 and 425. The L02 RecirculatorIn temperature (P1925T) rose above -291 DGF from 12.0 to 13.0 minutes duringRun 424 with a maximuwm temperature of -289 DGF. The temperature remained warm-er than -291 DGF between 13.0 and 13.4 minutes during Run 425 with a maximumtemperature of -290 DGF. The L02 topping valve was not opened until 14.3 min-utes during Run 426 and remained full open (25 to 28 GPM) until 20.25 minutes.The L02 Recirculator In temperature (P1925T) rose above -291 DGF at 11.5 min-utes and remained there until 17.6 minutes.

Sequence III pressurization was not initiated during these runs. Tank pressureswere maintained within the prescribed limits in all other sequences.

This document contains information affectng the national defense of the United States within the meaning of the Espionage Laws, Title 18,USC. Sections 793 and 794 The transmission or the revelation of its contents in any manner to an unauthorized person is prohinited by law,

FORMNO A7o2 2 -0LmUNCLASSF!ED

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'A ONFf DE TIALAddendumCON VAIR ASTRONAUTICS PA 2

1Siumary (Cont.'med)

T"he L02 boiloff valve ?IN 27-PO5Pg-8ll op~erated satisfactorily during Run 423However, during Runs 424, 425 ana 426, the Lfl2 boiloff valve closed light onthe Danel failed to cycle during initial tankinR? when visual observationindicated that the valve cycled. This probiex 13 under investigation'.

This document contains infor, on affecting the national defense of the Uoited States within the meaning of the Espionage Laws, Title 18,USC. Sections 793 and 794 The transmission oi the revelation of its contenits in any manner to an unauthorizrcd person is prohibited by law

FC',M NO A 702 2 CUO-N"" -- t -NT IA L

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ON iDENTIALAddendumCONVAIR ASTRONAUTICS rML 3

S3ETION 2

I Fuel Ioading Systen

The Fuel leading Systea loaded satisfactorily at IOC flow rates&Wing Runs 423, 424p 425 and 426 . T-he fuel rapid load wave was openedmnually by the console operator durng Run 423 due to a premature Acoustica90 fuel probe pickup, reventing the rapid load valve from opening inautcmtic uence.

The following table aswirises the fuel loading system data and additionaldata for Runs 423 and 424 are shown in Figures 3 and 2.

Ran No. Termlination Time Max. Flow Rate Max Weight Loaded

423 6.62 *4600 76,860424 6.78 *)600 76,920425 6.75 *4600 76,960126 *6.15 *4600 76,910

* Calculated over one minte interval from FUF TANK HD (Ul9O2P)**'Fuel load termnation time lesei than normal due to the fuel cone -not

being drained pior to Run 426.

This document contains information affecting the national defense of the United States wthin the meaning of the Espionage Laws. Title 18,US(C:. Sections 793 and 794 The transmission or the revelatior of ,ts contents in any mariner to an unauthorized person is prohibited by law

ORM No A,702 2CGft V

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SCONfWW-ENJALAde=CONVAIR ASTRONAUTiCS PL L

SECTION 3

Liquid Oxygen Loading System

The L02 Loading System satisfactorily performed loading at 10C flow ratesduring Runs 423, 424, 425 and 426. The 102 rapid load valve closed at 9.20nmtes during Run 425 (approximately the 68% L02 level) when the 90% AcousticaL02 probe picked up prematurely. The rapid load valve was opened at 9.43mintutes zunally by the console operator and loading continxued.See the Report !1 1L299 for detailed discussion of the engine 102 tank ffl3time.

The following table summiarizes the 102 Loading System dat.

Run No. Termination Time M(ax. i'-,i. Rate W Wehtaded

4-23 11-85 *5900 17540424 11.42 *5900 12,4425 **12.12 *5 90i) 172,630426 11-113 *5900C 1.729,630

*Calculated over one minute interval from LO? TK HD 0t1901P).** 12 load termination time morem tla& normal due tc the L02 rapit l-ad

valve closing for 0,23 mtnutets d~uring rapid loal,

L.02 Toppingz Syatems

The 1.02 Topping System perfoxillnce was unsatisfactory during htun 4i233. TheL02 topping valve did not open duhe to x.ist in the valve positioner, oaauselby condensation. The valve poaitioner was reworked prior to Run 4.24. Tne-L02 Recirculator In temperature (P1925T) rose above -291 DGP at Ll.5 Minttesand remained above that temperature until start of L02 drain during Run 1123.

The performance of the 102 Topping S&ytam aur-.Ung Runs 4264,25a and 426 v.,satisfactory. The 102 topping v,&Ive on Run 424 remained fuill open (2,6 GPY,)during the thirteen minute toppig hold becase L02 LOU STOP was signe! .edby the 99% L.02 level probe. The weight increase of L02 was 1,020 poundaduring thie hold, The L02 Recirculator Inteiuperature (P1925T) rose above-291 DO? at 12.0 -inutess and remained until 1.3.0 minutes. The nmimum temiperature reached was -=289 DO?,

The 102 topping valve remained full open K.. OWK) on R~un 425., throughoutthe run and the 6.5~ minute 1.02 topping hold. The L.02 Recfrculator In tem-perature (P1925T) remained warmer than -291 DO? from 13.0 to 13.4 inuteswith a maximm temperature of -290 DO?,

This document contaiiis information affecting the national defense of thP United States within the meaning of the Espionage Laws, Title 18,USC, Sections 793 and 794 Thn transmission or the revelation of its contents in any manner to an unauthorized person is prohibited by law

f OM o A70 2CG-N-F - " -TA L

Page 10: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

tHNfFHNTIALREPORT IM 1299

CONVAIR ASTRONAUTICS rPu 5

The W2 topping valve was not opened until 14.3 minutes during Run 426 andremained open until 20.25 xminutes (maxim flow rate 28 GPM). The L02 Recir-culator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes.

See graphic presentation for details on L02 Recirculator In temperature

(PI925T) for Run 423, 424, 425 and 426 (Fgures 5, 6, 7 and 8).

002 Sampling System:

002 samples were taken during L02 tanking and detanking on Runs 423, 424 and425, but not on Run 426.

The samples during Runs 423, 424 and 425 were taken at specified levels fordetermination of UN2 contamination. See Table I.

This document contains ,nformation affecting the national defense of the United States within the meaning of the Esp onage Laws Title 18USC Sections 793 and 794 The transmission or the revelaton of is contents in any manner to an unauthorized person is prohibited by law

fuRM NO A 702 2

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CMkNFff 0" LA AddendumREpIMT 1299

CONVAIR ASTRONAUTICS PAIr 6

SECTION 4HE/IN2 LOADING SYSTE

HE/LN2 system performance wa., satisfactory during Run 423. Booster bottletemoeratuare and pressure reauirements for 65-2 were achieved during this run.Helium load start was delayed 3 minutes after fuel load start as planned.This is the fourth consecutive run on which 65-2 requirements have beenachieved. LN2 high flow rate was lowered t- 86 GPM for this run. The LN2storage tank pressure was 88 PSIG.

The uorner and lower booster bottle temperatures at 13 minutes were -295 DGFand -304 DGF respectively. The lower bottle temperature (F1297T) indicated-326 DGF Just prior to helium dump. This is an impossible value, althoughit repeats data acquired during Run 422. This discrepancy is well withinallwable instrumentation error and the data can be considered reliable. Evenif an arbitrary correction factor of + 5 DGF is applied to &II values of thisparameter, the datm remains reasonable through the run and 65-2 requirementshave still beer achieved.

The characteristic droop in booster bottle pressure was repeated during thisrun. The attempt to remedy the problem by manually exercising PT-21 justprior to the run did not achieve the desired results. This problem is stillur der investigation.

The inline heat exchanger performance was satisfactory. No of the threetemperature measurements required for an evaluation of the heat exchanger\Fl744T and Fl91OT) were obtained. Helium temperature at the stub-u- (FI89 4 T)was not obtained due to excessive recorder noise durinp the run. The heatexchanger is still under evaluation. See Figure 9 for heat exchanger data.

HE/LN2 system performance was satisfactory during Run 424 although heliumloading was not attempted. The bottles were precharged to a low oressure (toorevent formation of a vacuum) and LN2 was loaded to simulate engine compart-ment atmosphere.

HE/LN2 loading was not attempted on Runs 425 and 426.

See Table 2 and time slice tab for HE/LN2 data.

This document contains information affecting the national defense of the United States within the meaning of the Espionage Laws T'tle 18,US,.', Sections 793 and 794 The !,ansmission or the revelation of its contents in any manner to an unauthorized person is prohirited by law

iORM NU A 702 2 C-o-- i----K I.-~.

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101 299

CONVAIR ASTRONAUTICS ri 7

SECTION

Convair PropellAnt k-ading Control System

Convair PLCU system,

The Convair Propellant Loading Control System was not installed for theeeruns. The unit was B'd prior to Run 419 and has been sent to San Diego.The fuel density was 50.2 on Test 425 and 426. N fuel samples were takenon Rm 423 and 424 so a fuel density of 50.3 lbs. per cu. ft. was assumed.

I Convat W Syse:

The Convair P9 syste operated in an open loop configuria~icin during Run 425ti'ough eThe error ratio demod signal (UIO91V) agreed within % o t re

other level sensing systems at the 90% level tat -ehce a 4% error P.-, the100% level. This error at the 100% level is due to calibration setting -Jthe U unit This system was used only for back-up duriig these testz 6c

r- -*tept will be made to correct this wntil c pletion of the presenx:series of tests.

This docum len! ,ontais informaton affecting tle national defen~e of the Jn

ted rates winin the meanng of the Esponage Laws Title 18

USC Sec',no *93 and 794 le transrr,ssor o' !he revP'afon ,If Is contents ,n ary marine to an unauthorized person is pohbJtec ny 3A

'RY N, A 70?2 2CO-N-HD-EANT--tL

Page 13: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

CON~FI~FN 4-kLAddendumNp"TR! 1299

CONVAIR ASTRONAUTICS r~r 8

MOfTION 6

Acoustica Propellant Loading Ccntrol System

Acoustica Dropellant loading control system performed unsatisfactorily duringthe fuel loading sequence of Riun 423. The Acoustica 90% fuel probe signalledranid load stop at 1.9 minutes which locked the system out of an automatic ra-pid fill sequence. k mr-ual loading sequence was initiated at tais tim~e andfuel and L02 tanking were continued. After exceeding the level of the 90%probe the au~tomnatic fill sequence was again initiated and performed satisfac-torily for the remainder of the run. Post test examination of this probe showedthe crossover imoedence to be out of tolerance. it is felt that an excessivelyhJLgh temperature .".n '*e 0~p of the fuel tank may- h-ve some effect or the crystalin the Acoustica n-obts. Table 3 s)bowt the temperature during Runs 417 through424. Post te-st examiination revealed the L02 9.% probe burned out, The Acous-tica q9% probe wil be used for fine fill cutoff for the remainder of the Acous-tica controlled nans.

The Acoustica Dropellant loading control system n-rforned satisfactorily onRun 4~24 with good agreement to the levels indi ated byr the other nropellantsensing systems.

On Run 425 the Acoustica system perfo)rmed unsatisfactorily during the L02 lodd-ing sequence. The Acoustica 90% probe prematurily s~gnalled L02 load stop whenthe level was 68%. L02 tanking was corntinLed Using thie manual loading orocedure.Post test examination of the 90% L02 proce t-nu' control unit showed the sensiti-.vity to have drifted from its original set~ing. Tine current at the datafax con-trol unit had to be increased to oroduce at L02 sensitive sensor.

The Acoustica oropellant loading contrj systen performed satisfactorily oilRun 426. The Acoustica system is compared to the other sensing systems inTables 4 through 7 for these tests.

This document contains information .Aecting the nationai defense of the United Stotes wthin the meaning of the Espionage Laws, Title 18,USC, Sections 793 and 794 The ttansmi ~sion or the revelation of its contents in any manner to an unauthorized person is prohibited by law,

FORM NO A 702 2

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C~flfPENIT~tAddend=m*EPOR Di 129

CONVAIR ASTRONAUTICS PUE 9 ___

SECTION7

Missile Pressurization System

The missile tank pressurization system performance was satisfactory duringRuns 4s239 424, ij25 andi 426. Sequence III pressurization was not initiatedduring these runs. However, tank pressures were maintained within the pre-scribed limits in all1 other sequences.

Operation of the W02 boiloff valve P/N 27-.80586-811 was satisfactory duringRun 423. Daring Runs 4~249 4~25 and 4~26 the L02 boiloff valve closed lighton the panel failed to cycle whben visual observation indicated

that the -mlxv cycled. It is felt that either the valve is not completelyclosing or the closed microWtch is intermittently failing under conditionsof high-venting such as is experienced during initial chilldovn, This pro-blem is under investigation.

This document contains information affecting the national defense of the United States within the meaning of the Espionage Laws, 'Itle 18,

USC, Sections 793 and 794 The transmisson or the revelaticin of its corl.nts in any manner to an unauthorized person is prohibited by law

FOMNO A 702 2 CJ R

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C4N DNTIAL Addenda.IEPUT 1 299

CONVAIR ASTRONAUTICS PGE__

SETION 8

Oround S2 port Equirent

The performnce of the ground support equipent during Runs 23, 424, 425and 426 vas satisfactory.

This document cintains information affecting the natioia, defense of the United States within the meaning of the Espionage Laws, Title 18,

USC Sections 793 and 794 The transmission or the reve,ation of its contents in an manner to an unauthnrized person is piohib-ted by law

PPY N,2 A 70? 2 CW D N- [1 L

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GON-L .ENTI A L _,,,, __',-

lal 125?

CONVAIR ASTRONAUTICS P*L _

SKTION 9

Data

In the following tabulation of time slice data an instrumentation deiat~icnor v Ifunction is noted by a nurber/letter cofbination in place of a da-avalue. For exlanation see Instrumentation %alfunction Code, page 34.

I

This docjment contans information affect~n :he rud ona deefen,. f ' e iJr, *t "tates witrin ,e mean ng of the ESPIOIld5 , La2 s T t'P I

USC Set-ons 793 and 794 The transmission c, tIe rp, ,dtion of is co~tL'ts n any manner, to an unauthorized person ,S prohb,!e. Dy aA

Page 17: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

G"4fJ N TI A L Aid

CONVAIR ASTRONAUTICS P~c,__

1-95 423 DATE 08-04-59

TIME IN MINMCHAS # DESCRIPTION UNIT REC 0 3 5 8 11 13

I1001P LO2 TANK HEL!UM PSIG L/;% 1.8 3.6 3.0 3.0 2e9 3.0FIOO3P FUEL TANK HELIUM PSIG LIN 10.1 28.8 27.2 58.1 58.3 p8.4F1066P G02 BO LN @ ELBOW PSIG L/N 2.3 2.1 2.3 2.6 2.6 2.8F1246P B TK HE BTLS Hi PSIG RX 13C 100 1250 2200 2780 3070F1248P S T' HE BTLS Hi PSIG BRN 280 280 1250 2155 2770 3030F1291P S CTL BTL 41 PSIG BRN 290 290 1220 2180 274C 3060F1770P LN2 STK ULL PSIG LIN 0 89 89 89 88 88F1952P L02 STOR TK PR PSIG BRN 0 19 19 106 106 106F1953P FUEL STORAGE TK PR PSIG BRN 1ii 113 117 117 118FI1O5R LN2 FLOW GPM L/ C 84 86 85 85 87IF1004T FUEL TANK HE DGF BRN 59 133 88 88 87 88F1064T G02 B @ ELBOW DGF BRN 92 104 -227 -203 -210 -267F1247T B TK HE BTL DGF BRN 83 34 -136 -262 -288 -295F1290T SUS CTL HE BTLS DGF BRM 99 96 90 51 28 22F1297T B TK HE BTLS DGF BR' 82 19 -156 -279 -298 -14F1739T FUEL PRESS GAS DGF BRN 90 72 54 58 60 34F!744T HE-LN2 HT EXCH OUT DGF BRX 27 29 -300 -310 -310 -3VcF1805T PRESS GAS MAN DGF BRN 8i 79 79 66 55F1894T HE LINE AT STUB UP DGF BRN 2E 2E 2E 2E 2E 2iF1910T IN LIN.E EXT OUT D3F L/% 40 -5 -243 -260 -262 -263N1980T TEMP TO SAMPLE BTL DGF 3RN 69 61 60 56 53 L;NI983T FULL FUEL PRESS BTL "3F SRN 34 95 94 92 9P100IP BI L02 PUMP IN PSIG L/N 0 3.8 4.7 18.7 26.4 2.-.3P3672P VERN FUL TK DIF FiD BRN 0C9 1.76 0.84 1.20 112 .n35

Pl6e2P PRESS DIF ON L02 TK PlD SRN C*C2 0.02 0.03 0.02 C 68 2 ['P1814P L02 TPG VLV PD BRN !,2 7.1 15.2 1.02 76 ".P18ibP L02 SUBCOOLER PID BRN -0.4 10 4 0.20 0&5' -c30

ENG L02 TK PR PiD BRN 0a15 4.4 5.0 16.0 20 ".0 5P1900P LAUNCHER INLET L02 PSIG BRN 3 21 15 66 C? 1iP1908P PR DIF FUEL TK P- SRN -. 01 0 0.67 1si8 ioi! .6P1950P LAUNCHER INLET FUEL PSIG :/N 8 79 40 35 37 39P1245R T SYS FUEL FR GPM L/N 0 4060 380 0 C 0P1020T 81 L02 P IN DGF 8RN 76 7B -293 -292 -289 -25P1054T 32 L02 P IN DGF BRN 7B -291 -292 -296 -28- -Z79P1530T SUS L02 P IN DGF BRN 78 -292 -292 -280 -27t -275P1700T FUL STK DISCH DGF BRN 90 90 88 88 90 58P1862T L02 SUBCOOLER OUT DGF BRN 43 -z2 -43 -41 -6 4P1869T L02 TPG DISCH DGF BRN 79 79 27 33 40 42P1887T ENG COMP AMB BYCONE DGF BRN 85 76 65 54 46 ! 3P188T VERN CTL MAN ENV DGF BRN 91 90 87 82 77 73P1889T VERN CTL MAN METAL DGF BRN 90 88 87 82 77 73P1903T LAUNCHER L02 IN DGF BRN 7B -198 -244 -265 -279 -266P1904T B2 L02 PMP VOL EXT DGF BRN 90 09 77 67 5,+ 46

. .,nt 3 s i P a i -,r', of The Esonage Laws T IS

AO f~t t L0t

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CO..N~iDN1IIA..[REPORT.L329____ -

CONVAIR ASTRONAUTICS A E

1-95 423 DATE 08-04-59

TIME IN MINMEAS if DESCRIPTION UNIT REC 0 3 5 8 11 13

P1905T BI L02 PMP VOL INT DGF BRN TB -287 -287 -276 7B 7B

P1906T 82 L02 PMP VOL INT DGF BRN 7B 78 7B 7B 7B 7B

P1907T B1 L02 PMP VOL EXT DGF BRN 77 77 70 54 43 35

P1912T LAUNCHER L02 OUT ,GF BRN 30 30 -300 -313 -317 -319

P1925T L02 RECIRC IN D~GF BRN 78 -295 -293 -298 -292 -287

U1901P L02 TK HEAD %FUL BRN 0 0.90 6s2 32 95 100

U1902P FUL TK HEAD %FUL BRIN 0 39 46 100 100 100U1091V ERROR RAT DM00 OTP VrC BRN 0 4

This document contains nforrjton affecting *tlie natfm)al defense of the United States withip the meaning of the tspionage l~aws Title 18

USC Secoins 793 and 794 The t'ansrn,s, o, the revelation of s contents in any manni-r to an unduthorized persor is pirh:biecl bv la.y

SA 702 2 60NFtDEN +A

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RE 1 1299CONVAIR ASTRONAUTICS rAGE __

1-95 424 TIME SLICE DATA

TIME IN MINMEAS # DESCRIPTION UNIT 9EC 3 5 8 11 13

F1OiP L02 TANK HELIUM PSIG L/N 2. 3.6 2.5 2.4 2.1 2.4

IF1003P FUEL TANK HELIUM PSIG '/ 1..2 2E 2%,1 56 58.2 58.2

F1066P G02 BO LN @ ELBOW PSIG ',N 2. 2.2 2.2 2.3 2.4 2.7

F1246P B TK HE BTLS Hi PSI3 2"t- 330 200 150 90 90 90

F1248P S TK HE BTLS Hi P31 BR: 45C '+30 430 420 410 410

F1291P S CTL BTL Hi PSIG BRN 47C 470 460 460 450 450

F1770P LN2 STK ULL PSIG L/% 3 90 90 89 88 88

F1952P L02 STOR TK PR PSIG ER! n 21 21 106 107 107

F1953P FUEL STORAGE TK PR PSIG BR: Q 111 115 117 118 118

F1105R LN2 FLOW GPM L,'N 86 84 86 86 84

F1004T FUEL TANK HE CGF BRN 1'5 138 88 88 88 88

F1064T G02 BO @ ELBOW DGF 8RN 99 -3C -227 -204 -204 -228

F1247T 8 TK HE BTL DGF 8AN 64 21 -139 -304 316 317

F1290T SUS CTL HE BTLS DGF BRN Th ?9 95 89 83 78

F1297T B -K HE STL5 DGF BRN 9i 16 -184 -317 -319 -320

F1739T FUEL PRESS GAS DGF BRN 94 62 43 49 51 53

F1744T HE-LN2 HT EACH OUT DGF BRN -L -19 -31 0 10 16

F1805T PRESS GAS MAN DGF BRN 9i -9 77 66 55 55

F1894T HE LINE AT STUB UP DSF SRN 7B 7B 78 7B 7B 7B

F1910T IN LINE EXT OUT DGF L'N -15 -85 -160 -117 -105 -102

N1980T TEMP 10 SAMPLE BTL DGF ER.N )4 '4 71 64 58 59

N1983T FULL FUEL PRESS BTL DGF 5RN 93 94 90 90 88 88

P0O0iP B L02 P)MP IN PSIG BRN 13 5.3 6.3 20.8 28 28

P1672P VERN FUL TK DIF PID FRN 7F

P1682P PRESS DIr ON L02 TK PID BRN -o0i 0 0 0 .76 1.5

P1814P LOZ T PG VLV PID BRN -3.4 .5 5.2 10.5 19o7 19.4

P1816P L02 bUBCOOLER PID BRN -o3 3 5 7B

P1900P LAUNCHER INLET L02 PSIG BRN 2 23 15 65 38 7

P1908P PR DIFF FUEL TK PID BRN .01 0 .65 1.17 1.17 1.17

P1930P EN3 L02 7K PRESS PID BRN 1,4 3.9 4el 10.7 13.3 13.3

P1950P LAUNCHER INLET FUEL PSIG L,'N 8.9 83 40 31 30 36

P1245R T SrS FUEL FR GPM Li' C 4230 380

P1020T B1 L02 P IN DGF BRN 70 -292 -293 -296 -290 -299

P1054 2 L02 P IN DGF RN 70 -290 292 -296 -284 -311

P1530T SUS L02 P IN DGF BRN 7B -?92 -291 -281 -277 -277P1700T FUL STK DISCH DGF BRN 38 90 88 88 88 88

P1862T L02 SUBCOOLER OUT DGF BRN -16 -211 -268 -284 -293 -293

P1869T L02 TPG DISCH DGF BRN 79 -81 -241 -264 -270 -270

P1887T ENG COMP AMB BYCONE DGF BRN 88 78 66 55 50 48

P1888T VERN CTL MAN ENV DGF BRN 95 94 92 88 85 82

P1889T VERN CIL MAN METAL DGF BRN 94 94 92 88 58 82

P19031 LAUNCHER L02 IN DGF BRN 7B -215 -256 -269 -275 -268

P1904T B2 L02 PUMP VOL EXT DGF BRN 92 90 76 65 55 50

Thi, documert contaris 'nlorrtnj.i affer tg the national deleit of the Int tares witth n tre meaning of the [Epion -p Laws, Title 18.

'ISO Sect.or, ;93 and 7(4 The t,nsnssion or th 'eiation of its conitert',. an,, manner to an unauthoriied person is pohibited by iaw

A 7C0 2N 4FNT4PDN TA-L

Page 20: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

CONVAIR ASTRONAUTICS _E15

1-95 424 TIME SLICE DATA

P1905T 81 L02 PUMP VOL INT DGF BRN 78 -287 -286 -276 7B 7BP1906T B2 L02 PUMP VOL INT DGF BRN 78 7B 7B 7B 7B 7BP1907T 1 L32 PUMP VOL EXT DGF BRN -17 -33 -31 4 8 10P1912T LAUNCHER L02 OUT DGF BRN 85 85 72 57 45 40P1925T L02 RECIRC IN DGF BRN 7B -294 -293 -298 -295 -293U1901P L02 TK HEAD %FUL BRN 0 2 9 31 96 100U1902P FUL TK HEAD SFUL BRN 0 46 92 100 100 100U1O91V ERROR RAT DMOD OTP VDC BRN 0 3.2

Tf s document contains informaton affecting the natonal defer,;e of the United States within the meaning of the Espionage Iaws, Title ]8USC Secton, 73 and 794 The transmsson or the 'eveijton of its cootent% in an manner to an unauthorized person ,s prohioited by faw

FJRM No A 7022 LOfft-E -TfAL

I= m

Page 21: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

1u 299CONVAIR ASTRONAUTICS ___ 16

11-95 425 DATE 08-06-59

TIME IN MINIMEAS # DESCRIPTION UNIT REC 0 3 5 8 11 13

F1001P L02 TANK HELIUM PSIG L/N 23 3.0 2.8 2.8 2.6 2.8F1003P FUEL TANK HELIUM PSIG L/N 9.5 27.8 26.0 56.2 56.5 56.5F1066P G02 BO LN ? ELBOW PSIG L/N 2.1 1.8 2.2 2.4 2.3 2.8F1246P B TK HE BTLS Hi PSTG BRN *F1248P S TK HE BTLS H1 PSIG BPN *F1291P S CTL BTL Hi PSIG BRN *F1770P LN2 STK ULL PSIG L/ *IF1952P L02 STOR TK PR PSIG BRN 0 20 20 107 107 108F1953P F'EL STORAGE TK PR PSIG BRN 6 107 111 113 114 114F11O5R LN2 FLOW GPM L/N *F1004T FUEL TANK HE DGF BRN 120 132 90 88 88 88F1064T G02 80 @ ELBOW DGF BRN 104 112 -229 -203 -189 -197F1247T B TK HE BTL DGF BRN *F1249T S TK HE BTL DGF BRN *F1290T SUS CTL HE BTLS DGF BRN *F1297T B TK HE BTLS DGF BRN *F1739T FUEL PRESS GAS DGF BRN 95 74 58 61 65 65F1744T HE-LN2 HT EXCH OUT DGF BRN 86 86 86 86 86 86F1805T PRESS GAS MAN DGF BRN 85 85 85 73 62 62F1894T HE LINE AT STUB UP DGF BRN *F1910T IN LINE EXT OUT DGF L/NN1980T TEMP TO SAMPLE BTL DGF BRN 74 4 72 67 64 64N1983T FULL FUEL PRESS BTL DGF BRN 95 96 95 94 92 93PIOOiP B1 L02 PUMP IN PSIG L/N 2.0 7.0 6.8 21.6 29.0 30.1

L02 TK VENT PID BRN 0 0s59 0 8.45 11j6 11.7P1682P PRESS DIF ON L02 TK PID BRN 0.01 0.01 0.02 0.02 0&02 1.48P1814P L02 TPG VLV PID BRN -7&1 1.5 5.6 10.1 19.5 19.1P1816P L02 SUBCOOLER PID BRN 2.3 2.3 493 20.3 20.2 20.3P1900P LAUNCHER INLET L02 PSIG BRN 3 19 14 64 36 8P1908P PR DIFF FUEL TK PID BRN 0.3 0 0.6 1.2 1.2 1.2P1930P ENG L02 TK PR PID BRN 2.9 7.7 77 19.6 24.1 24P1950P LAUNCHER INLET FUEL PSIG L/N 10 81 41 33 36 38P1245R T SYS FUEL FR GPM L/N 0 3870 400 0 0 0P1O20T B1 L02 P IN DGF BRN 78 -292 -293 -293 -292 -288P1O54T B2 L02 P IN DGF BRN 7B -289 -293 -297 -288 -307P1530T SUS L02 P IN DGF BRN 78 -292 -292 -281 -278 -277P1700T FUL STK DISCH DGF BRN 95 90 90 90 90 90P1862T L02 SUBCOOLER OUT DGF BRN -88 -216 -263 -231 -286 -285P1869T L02 TPG DISCH DGF BRN 73 -5 -239 -266 -276 -276P1887T ENG COMP AMB BYCONE DGF BRN 93 97 93 90 89 89P1888T VERN CTL MAN ENV DGF BRN 100 103 103 103 100 100P1889T VERN CTL MAN METAL DGF BRN 100 100 100 100 100 100P1903T LAUNCHER L02 IN DGF BRN 7B -215 -247 -269 -273 -274

* LN2/HK NOT LOADED THIS RUN.

This document ontas information affectng the national defense of the United States within the meaning of the Espionage Laws, Title 18,USC Sections 793 and 794 The transmission or the revelation of its contents in anv marner to an unauthorized person 13 prohibited by law

)9Y ANA A 7012 2 -& - _kT A L

Page 22: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

__ CON FIDENTIAL dmt

CONVAIR ASTRONAUTICS pASI 17

1-95 425 DATE 08-06-59

TIME IN MINMEAS # DESCRIPTION UNIT REC 0 3 5 8 11 13

P1905T 81 L02 PUMP VOL INT DGF BRN 7B 7B 7B 78 7B 7BP1906T 82 L02 PUMP VOL INT DGF BRN 7B -287 -287 -276 7B 7BP1912T LAUNCHER L02 OUT DGF BRN 98 -185 -231 -248 -257 -233P1925T L02 RECIRC IN DGF BRIN -267 -295 -295 -298 -296 -291U1101P L02 TK HEAD %FUL BRN 0 2 7 30 90 100U1902P FUL TK H IAD %FUL BRN 0 45 92 100 100 100U1091V ERROR RAT OMOD OTP VDC BRN 2.5

*LN? !HE NOT LOADED THIS RUN.

This document contains informatiui affecting the national defense of the United States within the meaning of the Espionage Laws, Title 18,USC. Sections 793 and 794 The transmission or the revelation of its contents in a, manner to an unauthorized person is prohibited by law

F ORM NO A 702?2 CO N F11HATJIA L

Page 23: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

CON , ENT ALCONVAIR ASTRONAUTICS pM 18

1-95 426 DATE 08-06-59

TIME IN MINMEAS 4 DESCRIPTION UNIT REC 0 3 5 8 11 15

F1001P L02 TANK HELIUM PSIG L/N 2&4 4.0 2.4 2.8 2.5 2.8

F1003P FUEL TANK HELIUM PSIG L/N 8.9 26.8 25.3 55 55.2 55.3

F1066P G02 BO LN @ ELBOW PSIG L/N 2.2 2.1 2.3 2.4 2.4 2*5

F1246P B TK HE BTLS Hi PSIG BRN *

F1248P S TK HE BTLS Hl PSIG BRNF1291P S CTL BTL Hi PSIG BRNFi77OP LN2 STK ULL PSIG L/N *F1952P L02 STOR TK PR PSIG BRN 0 20 20 106 106 107

F1953P FUEL STORAGE TK PR PSIG BRN 7 111 115 117 II7 118FIO5R L012 FLOW GPM L/N *FiOO4T FUEL TA:K HE DGF BRN * 140 88 8f, 87 87

F1064T G02 BO @ ELBOW DGF BRN ** 1 -209 -179 -200 -259

F1247T B TK HE BTL DGF BRN *F1249T S TK HE BTL Di'.F BRN *

F1290T SUS rTL HE BTLS rGa BRNF1297T B TK HE BTLS DGF BRNF1739T FUEL PRESS GAS DGF BRN ** 66 58 60 63 66

F1744T HE-LN2 HT EXCH OUT DGF BRN 88 88 88 88 88

F1805T PRESS GAS MAN DGF BRN ** 82 82 64 56 61

F1894T FE LINE AT STUB UP DGF BRN *F191OT IN LINE EXT OUT DGF L/NN1980T TEMP TO SAMPLE BTL DGF BRN 69 76 7+ 73 69 65

N1983T FuLL FUEL PRESS BTL DGF SRN - 94 94 93 92 90

PIOOIP B! LC2 PUMP IN PSIG L/N 2c-3 7.O 7.0 22.2 28.3 31.3P1682P PRESS DIF ON L02 TK PID BRN ' 0 0 0.3 1,i 1.5

P1814P L02 TPG VLV PiD BRN -7*0 e.'.1 23.6 95.0 78 29.8

P1816P L02 SUBCOOLER PID BRN 0 0 -0.8 2.2 0.6 19.6ENG L02 TK VENT PID BRN C 0 0 93 12o6 :0#2

P1900P LAUNCHER INLET L02 PSIG BRN 2A 2A 2A 2A 2A 2A

P1908P PR DIFF FUEL TK PID BRN 0 0 0&8 I'& 1i2 1o2

P1930P ENG L02 TK PRESS PID BRN 5.2 7.8 7.9 21.9 24:) 23.4

P1950P LAUNCHER INLET FUEL PSIG L/N 9 8i 41 35 3P 41

P1245R T SYS FUEL FR GPM L/N C 383C 390 0 3 0

P1O20T B1 L02 P IN DGF BRN 73 -292 -292 -289 -:86 -275

P1054T B2 L02 P IN DGF BRN 7B -291 -293 -297 -285 -2tl

P1530T SUS L02 P IN DGF BRN 7B -287 -291 -280 -277 -C'8

PiOOT FUL STK DISCH DGF BRN * 92 89 89 89 88

P1862T L02 SUBCOOLER OUT DGF BRN w -26 -19 -41 -37 -209

P1869T L02 TPG DISCH DGF BRN * 30 35 26 28 -160

P1887T ENG COMP AMB BYCONE DGF BRN 127 125 120 114 108 103

P1888T VERN CTL MAN ENV DGF BRN * 136 134 132 131 129

P1889T VERN CTL MAN METAL DGF BRN * 136 134 132 131 129

P1903T LAUNCHER L02 IN DGF BRN -100 -206 -248 -274 -2*6 -277

* LN2/HE NOT LOADED THIS RUN.

** tRDER NOT TURNED ON AT ZERO TIME.

This document contains information affecting the national defense of the United States within the meaning of the Espionage Lawz, Title 18.USC, Sections 793 arld 794 The tiansm:ssion or the revelation of it3 contents in any manner to an unauthorized person is prohibited by tow.

SA 02 CNFtDE-N-tt --

Page 24: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

tM COaFDENTIALCONVAIR ASTRONAUTICS ,9

1-3 5'z6 DATE 38-06-59

TIvE 1% YINiMEAS # DESCzIPTION z\IT REC C 3 5 8 11 15

IP1904T 82 L02 PUMP VOL EXT 8GF OR%

IP1905T 81 L02 PUMP VOL InT DGF ERN 75 73 7B 78 7B 70

P1906T 82 L02 PUMP VOL INT DGF ORN 75 -286 -287 -276 72 78

P1907T B1 L02 PUMP VOL EXT DGF BRN 7F

P1912T LAUNCHER L02 OUT DGP 3RX ** -194 -232 -252 -252 -222

P1925T L02 RECIRC V; 3GF BRN 72 -295 -294 -299 -294 -281

U1901P L02 TK HEAD %FJL 2 RN 4 8 39 100 10

U1902P FUL TK HEAD SFJL. ERN 6 54 95 100 100 iC0

U1O91V ERROR RAT DMOD OTP VC 2Rh .2 2.6

SX2/1N NOT LOADED THIS RUN.• RECORDER NOT TURD 0N AT ZEO T;B,

This document contains informatiun affecting tWe national defense of the United States wthin the meaning of the Espionage Laws, Title 18.USC. Sections 793 ard 794 The tiansmison or the revelation of its contents in any manner to an unauthorized person is prolib,ted by ia*

FORM NO A 702 CO44-F4DEN-T1A L

Page 25: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

COETALCONVAIR , AS-RONAUTICS PAE_.

'1.1

1-95 423 SE DATA

TIME PE N 0 * EAS M DESCRIPTION ACT DEACT

000 2 N1901X F PREPRES 1 VLV CLSD X

0.00 N1912X FUEL LCAZ START SW X

0.00 47 N1925X L02 COCLDOWN ST SW X

0.00 48 N1926X L02 TK VE'T VLV CLSD X

0.00 58 tN1962X LN2 'E'"7 VV OPEN X

0.01 13 N1917X F GRD F/C "VLV CLSD X

0.01 72 N1895X LN2 5TK ,E\'T VLV NCL X

0.02 69 N1892X LN2 LOAD VLV C..SD X

0.03 9 N1913X F PRPEPRES VLV 1 OPN X

0.03 14 N1916X F GND F/: VL% OPEN X

0.03 70 N±B93X LN2 LOAD VLV CPN X

0*3 71 N1894X LN2 ST ;- VLV LSD X

0.38 8 N1912X FUEL LOLD START SW X

0.39 3 NI902X F FINE LCAD VLV CLSD X0.39 9 N19I3X F PREPFESS VLV I OPN x

0.39 11 P1966X F VSL F/D VLV CLSD X

0.40 2 N19OIX F PREPRES 1 VLv CLSD X

0.41 10 N1914X F FINE LCAD VLV OPEN X0.43 12 P1967X F MSL F/D VLV OPEN X

0.45 26 N1890X INTER PJL STK PRESS X

0.91 17 N1922X FUL RAPID LD SIGNAL X

1,63 71 N1894X LN2 STK P VLV CLSD X

1.90 27 N1969X AA FJEL 90% PROBE X

2.13 18 N1923X FUL RAPIC VLV CLSD K

2.17 15 N1919X F STK PRESS CLSD

2.18 4 N1903X FUL RAPID LD VLV OPN X2.39 43 N1906X L02 FINE LD VLV CLSD X2,9 50 N1930X L02 CGND F/D VLV OPEN X

2.39 64 N1968X L02 MSL F.D VLV CLSD X

2.40 49 N1929X L02 GND F/D VLV CLSD X

2.41 44 N1907X L02 STK P VLV A CLSL x

2.42 51 N1931X L02 FINE LD VLV OPEN X

2.42 63 N1967X L02 M..L F/D VLV C-N X

2.43 54 N1934X L RAPID LD VLV CLSD X

2o47 42 N1905X L RAPID LD VLV OPEN X

2.55 66 N1891X L02 NOT IN UPPER LN X

2.60 56 N1949X L02 LN LIQ DET/INTRM A

2o70 44 N1907X L02 STK P VLV A CLSD X

2.83 56 N1949X L02 LN LIO DET/INTRM X

3e03 68 F1897X FLIGHT HE 1 VLV CLSD X

3.05 68 F1897X =LIGHT HE 1 VLV CLSD X

3.52 56 N1949X L02 LN LIQ DET/INTRM X

4.02 56 N1949X L02 LN LIQ DET/INTRM X

4.51 4 N1903X FUL RAPID LD VLV OPN X

_ U+

C@NFhD-io

Page 26: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

ii REPORTCONIVAIR AS-RONAUTICS PAGE _21

1-95 423 SEQ DATA

TIME PEN # MEAS N DESCRIPTION ACT DEACT

4.58 18 N1923X FUL RAPID V.v CLSD X4.72 56 N1949X L02 LN LIC DEiT/I 7RM X4.73 79 P1899X AA PROBE @ STA 910 X5.04 15 N!919X F STK PRESS CLSD X5*06 78 P1898X HW PROBE C ETA 910 X6*61 6 P1999X MSL FUELEC 100% X

6.62 3 N1902X F FINE LCAD VLV CLSD X6.62 10 N1914X F FINE LOkD VLV OPEN X6.62 29 N1971X AA FUEL 1C0% PROBE X6.63 12 P1967X F MSL F/n vL.v OPEN X6.66 11 P1966X F MSL F/D VLV CLSD X6s68 14 N1918X F GND F/D VLV OPEN X6.70 13 N1917X F GRD F/C VLV CLSD X6.74 6 P1999X MSL FUELED 100% X6.75 29 N1971X AA FUEL 133% PROBE X6.94 44 N1907X L02 ST< P vLV A CLSD X

6.95 55 N1936X L02 LOA-,.,G PRESS X7*10 63 N1967X L02 MSL FiD VLV OPEN X7.24 76 P1896X HW PROBE @ STA 888 X7.26 79 P1899X AA PROBE STA 910 x

7.51 75 P1895X AA PROBE 2 STA 866 X7.51 79 P1899X AA PROBE @ STA 910 X8.19 77 P1897X AA PROBE @ STA 888 x8.93 37 P1690X HW PROBE c2 STA 700 X9.08 40 P1893X AA PROBE @ STA 793 X9.09 79 P1899X AA PROBE S STA 910 X9.19 77 P1897X AA PROBE e STA 8889.19 79 P1899X AA PROBE r STA 910 X9,36 77 P1897X AA PROBE @ STA 888 X9.43 38 P1891X AA PROBE , STA 700 X

9.80 31 N1973X HW LO2 RAPID SIG/90% X9.83 42 N1905X L RAPID LD VLV OPEN X9.89 54 N1934X L RAPIT LD V+' CLSD X

11.16 73 P1673X L02 ST TK FULL X11.85 33 N1975X HW L02 FIN SIG 99% X11.85 46 P1998X MSL L02 2 100%11.35 51 N1931X L02 FINE LD VLV OPEN X11&8J 43 N1906X L02 FiNE LD VLV CLSD X11.89 49 N1929X L02 GND F/D VLV CLSD X11.90 50 N1930X LO2 GND F/D VLV OPEN X11.98 66 N1891X L02 NOT IN UPPER LN X15.05 46 P1998X MSL L02 G 100% X

15,14 46 P1998X MSL L02 . 100% x15.56 43 N1906X L02 FINE LD VLV CLSD X

S-Y', A G22

Page 27: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

II RI : AMdenm

REOT 11299CONVAIR ASTRONAUTICS PACE -

1-95 423 SEQ DATA .. ..

TIME PEN # MEAS # DESCRIPTION ACT DEACT

15.58 51 N1931X L02 FINE LD V.-V OPEN X15.74 47 N1925X L02 CO L'DON ST SW X15.74 48 N1926X L02 TK VEIN- V'LV CLSD X15.75 51 N1931X L02 ;I , .. ,V OPEN X15.78 43 N1906X C2 7 1 ,E L- vLV CLSD X

NOTE

1. THESE PENS ACTIVATED THROUGHOJT T-nz TEST

7 N1911X EMER MISL PRESS COND16 N1921X FUEL LOADING PRESS22 N1956X FUEL STK ,'T VLV CLSD23 N1960X F MAiN ORN VLV CLSD24 N1961X F MAIN DRA VLV OPEN45 P1988X MSL L02 @ 95%52 N1932X L02 TCP v -'%, C.....53 N1933X L02 T4O CPEN57 N1951X PRESS DUCT FUEL SNSR59 N1963X L PAIN DPN v V CLSD60 N1964X L MAIN LRN VL OPEN

2v THESE PENS DEACTIVATED THROUGHOUT THE TESI

5 P1997X IS. FUELED 95%19 N1943X F LN LIQ DETIINTERM20 N1955X FUEL DRAIN START SW25 N1965X FUL DRAIN COMPLETE28 N1970X AA FUEL 95% PROBE30 N1972X AA FUEL 99G89% PROBE32 N1974X HW L02 BU 95% SIG3435 N1977X HW L02 TOPG COF SIG36 N1978X HW L02 EM SIG 100.2%39 P189?X HW PROBE @ STA 79362 N1966X L02 DRAIN COMPLETE65 N1889X INTER L02 STK PRESS67 F1896X LN2 INFLIGH! HE LOAD74 P1894X L02 95% EMERG COF

ThS document conaumi nfont of affe' ( I f ,iy nM on ,Ift!, of the ,' , States Atl. tip rmedl l (f the ESu 'or Igp Laws Ti1le 18

USC Sp:tlorf i] i ,'a, Th t " K 0 ", 1', f :I pw ,tson S p OO , 'd bf

A702 2 GG44H- -- H AL

Page 28: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

Id '-1-DE NT I A L dom

CONVAIR ASTRONAUTICS pAC2E3

11-95 424 SEQ DATA

TIME PEN # MEAS # DESCRIPTION ACT DEACT

000 8 N1912X FUEL LOAD START SW X

0.00 2 N1901X F PREPRES 1 VLV CLSD0.00 47 N1925X L02 COOLDOWN ST SW X0.00 58 N1962X LN2 VENT VLV CPEN X0.01 48 N1926X L02 TK VENT VLV CLSD X

0.01 72 N1895X LN2 STK VENT VLV NCL x

0.02 69 N1892X LN2 LOAD VLV CLSD X

0.03 9 N1913X F PREPRESS VLV 1 OPN X0.03 70 N1893X LN2 LOAD VLV OPN X

0.03 71 N1894X LN2 STK P VLV CLSD X

0.43 3 N1902X F FINE LOAD VLV CLSD X

0@43 8 N1912X FUEL LOAD START SW X

0.43 9 N1913X F PREPRESS VLV I OPN X

0.43 11 P1966X F MSL F/D VLV CLSD X

0.44 2 N19O1X F PREPRES I VLV CLSD X

0.44 13 N1917X F GRD F/D VLV CLSD X

0.45 10 N1914X F FINE LOAD VLV OPEN X

0.46 14 N1918X F GND F/D VLV OPEN X

0.47 12 P1967X F MSL F/D VLV OPEN X0.47 26 N1890X INTER FUL STK PkESS X

0.74 19 N1943X F LN LIO D9T/INTERM X

0,92 17 N!922X FUL RAPID LO SIGNAL1.47 71 N1894X LN2 STK P VLV CLSD x1.91 18 N1923X FUL RAPID VLV CLSD X

1.96 4 N1903X FUL RAPID LD VLV OPN X

2.09 15 N1919X F STK PRESS CLSD A

2.21 16 N1921X FUEL LOADING PRESS X2.22 43 N1906X L02 FINE LD VLV CLSD X2.22 52 N1932X L02 TOPPING VLV CLSD A

2.23 50 N1930X L02 GND F"D VLV OPEN X

2.24 49 N1929X L02 GND F/D VLV CLSD x

2.24 53 N1933X L02 TOPPING VLV OPEN

! 2.24 64 N1968X L02 MSL FiD VLV CLSD X

2.25 44 N1907X L02 STK P VLV A CLSD X2.26 51 N1931X L02 FINE LD VLV OPEN X

2.26 63 N1967X L02 MSL F/D VLV OPEN X

2.27 54 N1934X L RAPID LD VLV CLSD X

2.32 42 N1905X L RAPID LD VLV OPEN X

2.32 44 Ni907X L.02 STK P VLV A CLSD X

2.37 66 N1891X L02 NOT IN UPPER LN X

2.38 66 N1891X L02 NOT IN UPPER LN X2.40 56 N1949X L02 LN LIQ DET/INTRM X

2.41 56 N1949X L02 LN LID DET/INTRM X

2.42 56 N1949X L02 LN LIO DET/INTRM X

This document rontai, nfo iat-on affvrtrlg the nat :,.31 efpc St of the m, teJ State At , , the -ecin~nr f the Fsponge A T w

USC Setons 793 3 ) N The !ransm ss - or the eVplat n a c ute' St ,l ?I al nn ,n Antjth(; Ij j un'son 's ,r, b pe' e

Cq V A 702E2 G-9-NL LNTIAL

Page 29: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

C-N DNI[ 1299

-ONVAIR ilASTRONAUTICS

1-15 424 SE 'ATA

TI1E PE'4 V ASESCC7PTIC% ACT DEACT

2.75 56 N1949X L02 L', LI. )ET2'"TRM x

4o24 27 N1969X A FUEL 90% P:S=E x4.25 4 N1903X FUL RAPI -3 LV OPN x4o33 18 N1923X FUL RAPID VL.V C.SC X4.54 79 P1899X AA P TE S-L 9!Z X4.55 78 P1896X H%. PROBE 'S-- 910 X6.77 6 PI999X M.L C'E ED .. x

6.78 3 N1902X F F.'E LOAD ,Lv CLSD X6.78 5 P!997X MSL FUELED ;5% X6.78 10 UI914X F FINE L-AD /L OPEN X6.78 29 N1970X AA FUEL 95% PROBE X6.79 12 P1967X F YSL r/, 'LV OPEN X6.83 11 P1966X F -!SL F/D .'L CLBD X6.84 14 NI918X F G3% F/,, v, CPE'-P X6.84 76 P'896X mw PPO4E ? S- 688 X6985 79 P1899X A A P;aE S 91 x6.87 13 '!i?17X F GRD F'D -_, CSD X6.91 6 P1999X 'IS- FoELED 13C% x691 29 N1970X AA FeEL 95" PROBE X7.08 55 N1936X L02 LOADING P:ES X7.11 44 N1907X L02 STK P VLi A ZLSD X7.22 65 N1889X i-NTER -02 STK P:-EZSS x7e53 44 N1907X L02 S'< P Vi.V A CLSD X7o54 75 P1895X AA P :9E STA 866 X

7*55 44 N1907X LC2 5TK P V,.V A CLSD I7.55 79 P1899X AA PROBE Z TA 910 X8.20 77 P1897X AA PROBE @ ST 888 x8.95 ;7 P189 X Hw PROBE @ STA 700 X

9.07 40 F1893X AA PROBE 1@ STA 793 X

9.10 79 P1899X AA PROBE F STA 910 X

9.17 79 P1899X AA PROBE, S PA 910 X9.13 77 P1897X AA PRO6E ? STA 888 X

9.29 77 P1897X AA PROBE @ STA 098 X

9,3* 38 P1891X AA PROBE @ STA -00 X9.82 31 N1973X HW L02 RAPID SIG/90% X9.90 42 N1905X L RAPID LD 'ILV 'OEN X9.91 54 N1934X L RAP,O LD VLV CLSD X

11.40 33 N1975X HW L02 FIN SG 99% X11.41 46 P]998X MSL L02 @ 100% X11.42 51 N1931X L02 FINE LD VLV OPEN x11,44 43 N1906X L02 FINE LD VLV CLSD X

11s4 44 N1907X L02 STK P VLV A CLSD X

11.45 49 N1929X L02 GND F/D VLV CLSD x11.46 50 N1930X L02 GND F/D VLV OPEN x

Tni document contains nfnrmaton affeong the nj!' ra: defense of the t,' ted Slates 01hn the mranng of tht Espionage Laws Tdile 18uSC Sertoni ' aid 794 Tfif trari m,ss on of the 'e Plaicn o

f i cL,n'e, ?, . .,m to an ,autharzed persoi is pohibite by law

,Y,,, A 702 2 C MOf1 ENT A L

Page 30: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

=-ON Fi DENT AddendE[P9T I 1.299

CONVAIR ASTRONAUTICS P____-

j1-95 424 SEQ DATA

NOTE

1. THESE PENS ACTIVATED THROUGHOUT THE TEST

7 N1911X EMER MSL PRESS COND

22 N1956X FUEL STK VT VLV CLSD23 N1960X F MAIN DRN VLV CLSD24 N1961X F MAIN DRN VLV OPEN

45 P1988X MSL L02 @ 95%57 N1951X PRESS DUCT FUEL SNSR59 N1 963X L MAIN DRN VLV CLSD

60 NI964X L MAIN DRN VLV OPEN

68 F1897X FLIGHT HE 1 VLV CLSD

2. THESE PENS DEACTIVATED THROUGHOUT THE TEST

20 N1955X FUEL DRAIN START SW

25 N1965X FUL DRAIN COMPLETE

28 N1971X AA FUEL 100% PROBE30 N1972X AA FUEL 99.89% PROBE

32 N1974X HW L02 BU 95% SIG

35 N1977X HW L02 TOPG COF SIG36 N1978X HW L02 EM SIG 100.2%39 P1892X HW PROBE @ STA 793

62 N1966X L02 DRAIN COMPLETE67 F1896X LN2 INFLIGHT HE LOAD73 P1673X L02 ST TK FULL74 P1894X L02 95% EMERG COF

This document contains nto'mation affoctiro the national defense of the Unted States within the meaning of the Espionage Laws, Title IS,

USC, Sections 793 and 794 The trans.nissiori or the eveldtion of ts contents in any marner to an unauthorized person is prohibite hy law

uRY NO A 7022

Page 31: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

AGG~Wl4E*iiAt _ _dnd[I EEPORT U 12x9

CONVAIR ASTRONAUTICS PUe 26

1-95 425 SEQ DATA

TIME PEN # MEAS N DESCRIPTION ACT DEACT

0.00 8 N1912X FUEL LOAD START SW X0.00 2 N1901X F PREPRES 1 VLV CLSD x

0.01 47 N1925X L02 COOLDOWN ST SW X001 48 N1926X L02 TK VENT VLV CLSD X0.03 9 N1913X F PREPRESS VLV 1 OPN X

0.45 3 N1902X F FINE LOAD VLV CLSD X0.45 8 N1912X FUEL LOAD START SW X

0.45 9 N1913X F PREPRESS VLV 1 OPN X0.45 11 P1966X F MSL F/D VLV CLSD X

0.46 2 N19O1X F PREPRES 1 VLV CLSD X0.46 13 N1917X F GRD F/D VLV CLSD X

0.48 10 N1914X F FINE LOAD VLV OPEN X

0.48 14 N1918X F GND F/D VLV OPEN X

0.49 12 P1967X F MSL F/D VLV OPEN X

0.53 26 N1890X INTER FUL STK PRESS X

0.76 19 N1943X F LN LIQ DET/INTERM X

0e94 17 N1922X FUL RAPID LD SIGNAL X

1.94 18 N1923X FUL RAPID VLV CLSD x1.99 4 N1903X FUL RAPID LD VLV OPN X

2.16 15 N1919X F STK PRESS CLSD X

2.23 16 N1921X FUEL LOADING PRESS X2.25 43 N1906X L02 FINE LD VLV CLSD X

2.25 52 N1932X L02 TOPPING VLV CLSD X

2.26 50 N1930X L02 GND F/D VLV OPEN X

2.26 64 N1968X L02 MSL F/D VLV CLSD X

2s27 44 N1907X L02 STK P VLV A CLSD X

2.27 49 N1929X L02 GND F/D VLV CLSD X

2.27 53 N1933X L02 TOPPING VLV OPEN X

2.28 51 N1931X L02 FINE LD VLV OPEN X

2.29 54 N1934X L RAPID LD VLV CLSD X

2.29 63 N1967X L02 MSL F/D VLV OPEN X

2.34 42 N1905X L RAPID LD VLV OPEN X

2.35 44 N1907X L02 STK P VLV A CLSD X

2.40 44 N1907X L02 STK P VLV A CLSD X

2.40 66 N1891X L02 NOT IN UPPER LN X

2.45 56 N1949X L02 LN LIG DET/INTRM X

2.53 44 N1907X L02 STK P VLV A CLSD X

2.78 56 N1949X L02 LN LIO DET/INTRM x3.00 36 N1949X L02 LN LIO DET/INTRM X

4.27 4 N1903X FUL RAPID LD VLV GPN X

4,27 27 N1969X AA FUEL 90% PROBE x4.34 18 N1923X FUL RAPID VLV CLSD X

4.70 15 N1919X F STK PRESS CLSD X

t7 5 78 P1898X HW PROBE @ STA 910 X

This document contdins itf maton affectng the nitional defense of the ' ited States with;n the meaning of the Espionage Laws, Title 18,

USC Sections 711 and 14 The transmssion or the revelation 0 iscon 's in anv mannt' to an unauthorized person is prohibited by law

RY N A 702 2 GGNZWD :*ffNttl

Page 32: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

CONVAIR ASTRONAUTICS Plgc27

1-95 425 SEQ DATA

TIME PEN # MEAS # DESCRIPTION ACT DEACT

475 79 P1899X AA PROBE @ STA 910 X

6#73 29 N1971X AA FUEL 10C% PROBE X

6.74 6 P1999X MSL FUELED 100 X

6.75 3 N1902X F FINE LOAD VLV CLSD x

6.75 10 N1914X F FINE LOAD VLV OPEN X

6.76 12 P1967X F MSL F/D VLV OPEN X

6.79 11 P1966X F MSL F/D VL*" CLSD X

6.81 14 N1918X F GND F/D vLV OPEN X

6.84 13 N1917X F GRD F/D VLV CLSD x

6.86 29 N1971X AA FUEL 100% PROBE X

6.87 6 P1999X MSL FUELED 100% X

7.05 55 N1936>' L02 LOADING PRESS X

7.08 44 N1907X L02 STK P VLV A CLSD X

7.21 76 P1896X HW PROBE F STA 888 x

7.22 65 N1889X INTER L02 STK PRESS X

7.26 79 P1899X AA PROBE @ STA 910 X

7.58 75 P1895X AA PROBE @ STA 866 X

7.59 79 P1899X AA PROBE @ ST" 910 X

9 8.21 77 P1897X AA PROBE @ STA 888 X

8.95 37 Pi890X HW PROBE @ ST4 700 X

9.10 40 P1893X AA PROBE @ STA 793 X

9.11 31 N1973X HW L02 RAPID SIG/90% X

9.14 42 N1905X L RAPID LD VLV OPEN X

9.17 31 N1973X HW L02 RAPID SIG/90% X

9.20 54 N1934X L PAPID LD VLV CLSD X

9.35 38 P1891X i, PROBE @ STA 700 X

9.43 54 N1934X L RAPID LD VLV CLSD x

9.50 42 N1905X L RAPID LD VLV OPEN X

10.03 42 N195oX L RAPID LD VLV OPEN X

10.08 31 N1973X HW L02 RAPID -IG/90% x

10.08 54 N1934X L RAPID LD VLV CLSD X

12o12 33 N1975X HW L02 FIN SIG 99% X

12.12 46 ?1998X MSL L02 @ 100%

12.12 51 N1931X L02 FINE LD VLV OPEN X

12.15 43 N1906X L02 FTNE LD VLV CLSD X

12.16 49 N1929X L02 GND F/D VLV CLSD X

12.16 50 N1930X L02 GND F/D VLV O?EN X

12.30 44 N1907X L02 STK P VLV A CLSD

16.66 73 P1673X L02 ST TK FULL x

This document contains information atfe,,ting the national defense of the United States within the meaning of the Fspionage Laws, Title 18,

USC. Sections ?93 and 794 The trinsmission or the 'evelaton of its contents in any manner to an unauthorized Person is prohibited by law

N

UW U i?

Page 33: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

CONVAIR ASTRONAUTICS PAE 28

11-95 425 SEQ DATA

NOTE

1THESE PENS ACTIVATED THROUGHOUT THE TEST

7 N1911X ENER 45L P?ESS COND22 N1956X FUEL STK VT '!L, CLSD23 N1960X F A:N DF V/LV CLSD24 N1961X F '1,A-% DR-N ILV OPEN45 P1988X MSL L02 2 95%57 N1951X PRESS- DUCT F -L SNSR58 N1951X LN2 VENT VLV' CPEN59 N!963X L MAIN DRN -!LV CLSD60 N1964X L MAIN DRN VLV' OPEN68 F1897X FLIGHT HE 1 'iLV CLSD69 N1892X LN2 LOAD VLV CLSD70 N1893X LN2 LOAD VLV OPN71 N1894X LN2 STK P VLvy CLSD72 N1895X LN2 STK VENT VLV NCL

2. THESE PENS DEACTIVATED THROUGHOUT THE T;-3'S

5 P1997X MSL FUELED 95%25 N1965X FijL DRAIN COMvPLETE28 N1970X AA FUEL 95% PROBE30 N1972X AA FUEL 99.89% PROBE32 N1974X HW4 L02 BU 95% S.C'35 N1977X HW L02 TOPG COF S-IG36 N1978X HW L02 EM SIG 100a2%39 P1892X HW PROBE @ STA 79362 N1966X L02 DRAIN COMPLEIE'.74 P1894X L02 ^75% ENIERG COc

Ths document con~a~ns inford,, at aaffecti'g the naional defense o!f tilnied St3teS within tre mnearig ft tic p'on'4 I aws Title 18,USL Sections 7,q3 aid /94 The tansrm sson or the 'evidjtcn of its cunter-t in n y nanne, ia in unauthot :,ed person is prohibitedl by law

RY %' A 02 2C0N-H-D-EAfI A L

Page 34: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

C -NEDN-T4A L AddendumREPORT IN 12" __ _

CONVAIR ASTRONAUTICS PAG[-29__

1-95 426 SEQ DATA

TIME PEN # MEAS # DESCRIPTION ACT DEACT

0.00 8 N1912X FUEL LOAD START SW X

0.00 2 N1901X F PREPRES 1 VLV CLSD X

0.00 9 N1913X F PREPRESS VLV 1 OPN X

0.00 47 N1925X L02 COOLDOWN ST SW x0.00 48 N1926X L02 TK VENT VLV CLSD X

037 3 N1902X F FINE LOAD VLV CLSD X

0.37 8 N1912X FUEL LOAD START SW X

0.37 9 N1913X F PREPRESS VLV 1 OPN x

0.38 2 N1901X F PREPRES 1 VLV CLSD X

0.38 11 P1966X F MSL F/D VLV CLSD X0.38 13 N1917X F GRD F/D VLV CLSD X

0.39 10 N1914X F FINE LOAD VLV OPEN X

0.40 14 N1918X F GND F/D VLV OPEN X

0*42 12 P1967X F MSL F/D VLV OPEN x

012 26 N1890X INTER FUL STK PRESS x

0.59 19 N1943X F LN LIO DETINTERM X

0.75 17 N1922X FUL RAPID LD SIGNAL X

1.60 15 N1919X F STK PRESS CLSD X

1.68 4 N1903X FUL RAPID LD VLV OPN X

1.78 18 N1923X FUL RAPID VLV CLSD X

2.04 43 N1906X L02 FINE LD VLV CLSD X

2.04 50 N1930X L02 GND F/D VLV OPEN X

2.05 49 N1929X L02 GND F/D VLV CLSD X

2.05 64 N1968X L02 MSL F/D VLV CLSD X

2.06 16 N1921X FUEL LOADING PRESS X2&06 44 N1907X L02 STK P VLV A CLSD X2.07 51 N1931X L02 FINE LD VLV OPEN X

2.08 54 N1934X L RAPID LD VLV CLSD X

2.08 63 N1967X L02 MSL F/D VLV OPEN A

2.12 42 N1905X L RAPID LD VLV OPEN x

2.14 44 N1907X L02 STK P VLV A CLSD x

2.21 56 N1949X L02 LN LIQ DET/INTRM X

2.21 66 N1891X L02 NOT IN UPPER LN X

2 o6 56 N1949X L02 LN LIQ DET/INTRM X2.77 62 N1966X L02 DRAIN COMPLETE X

? 28 56 N1949X L02 LN LIQ DET/INTRM X

4#04 27 N1969X AA FUEL 90% PROBE X

4.05 4 N1903X FUL RAPID LD VLV OPN X

4.12 18 N1923X FUL RAPID VLV CLSD X

4.34 79 P1899X AA PROBE @ STA 910 X

4.37 78 P1898X HW PROBE @ STA 910 X

4.61 15 N1919X F STK PRESS CLSD X

6.15 6 P1999X MSL FUELED 100%

6.15 29 N197'X AA FUEL 100% PROBE X

This document cu,:a,.s nfo'maton affecting the natonal 1etfnsp of the lnitd States within the meaning of the Espionage Laws, Title 18,

USC Sections ;q3 and 794 The , 3nsmiss in o ' c ! iPvP a)fi o is Colerds in any manner to an unauthorized person is p,olibited by law

RY N A 702 2 C& ffNAL

Page 35: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

C OrNfi af-NtIAt MONT ' 1299

CONVAIR A STRONAUTICS PACL.G__

1-i95 426 SE-DATA

TI>IE PEN -MEAS # DESCRIPTION ACT DEAC

6.16 3 N1902X F FINE LOA. .L, CLSD X6*16 10 N1914X F FI'.E L:4L' V -. OPEN X6e16 12 P1967X F 'ISL F/D VL'/ OPEN X6.20 11 P1966X F YSL F/- ',LV CLS) X6.21 14 N1918X F $ND F, VL' OPEN X6.24 13 N1917X F GR'j F/: VL, ,LSD X6.28 6 P1999X jL JEL:D 1-O% X6.28 29 N1971X AA FuEL 100% 0ROBE X6.42 55 N1936X 102 LOADING PKESS X6.42 78 P1898X HW FPOBE ? STA 910 X6o42 79 P1899X AA PROBE 2 Z'A 910 X6,46 44 N1907X L02 S'K P \ A CLSD x6.59 65 N1889X INTER L02 ST K PRESS X6.72 78 P1898X HW PROEE STA 910 X6.73 79 P1899X AA PRCRE C ST 910 X6.98 76 P1896X Hv. PROBE @ STA 888 X7e02 79 P1899X AA PROBE @ STA 91C x7.23 75 P1895X AA PROBE ? ST A 866 X7.23 79 P1899X AA PROBE @ STA 910 X7.87 77 P1897X AA PPOBE C STA 888 X8.58 37 P1890X HW PROBE @ STA 700 X8.78 40 P1893X AA PROBE , STA 793 X8.78 79 P1899X AA PROBE T A 910 X8.86 79 P1899X AA PRDBE C STA 910 X8.87 77 PI897X AA PROBE 2 STA 888 X9.08 77 P1897X AA PROEE @ STA 888 x9.12 38 Pi891X AA PROBE @ STA 700 X9.47 31 N1973X HW LC2 RAP'D SIGf90% X9047 42 N1905X L RAPID L) VLV OPEN X9s52 54 N1934X L RAPID LD V v CLSD X11.13 46 P1998X MSL LC2 @ 100% X11.13 51 N1931X L02 FINE LD ViLv OPEN X11l.6 33 N1975X HW 3-2 F N S11 99% X11.16 43 N1906X L02 FINE LD Vl-V CLSD X11.16 49 N1929X L02 GND F/D VLV CLSD X11.17 50 N1930X L02 3ND F/D VLV OPEN X11.27 66 N1891X L02 NOT IN uPPER LN X11.84 56 N1949X L02 LN IAC DET, INTRM X12.32 56 N1949X L02 LN LIQ DET/NTRM X13.19 44 N1907X L02 STK P VLV A CLSD X14.24 52 N1932X L02 TOPPING VLV CLSD X14.25 53 N1933X L02 TOPPING VLV OPEN X14.77 66 N1891X '-02 NOT IN UPPER LN X19.72 73 P1673X L02 ST TK FULL X

Thls doc ment rcntains infirrdtion affectinF the nat,orai defen~c of the Unitej States w0hin the meaning of the Espionage Laws Title 18.USC Secion£ '93 ard 'q4 The transm~ss n )r the e ijaton of ,,is cunten; in any any a ir t) an unauthop zed person is prohib-ted by law

5N, A 702 2 CON-4E-N IL

Page 36: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

COffDENTtAtCONVAIR ASTRONAUTICS ncJ __

, 1-95 426 SEQ DATA

TIME PEN # MEAS # DESCRIPTION ACT DEACTi

20.23 53 N1933X L02 TGPPI!;G VLV OPEN X20.25 52 N1932X L02 TOPP:%,5 V, CLSD X20*54 47 N1925X L02 C3OLCOlft ST S X

NOTE

1. THESE PENS ACTIVPTED THROUG-OLT THE TEST

7 N1911X EME? YSL PRESS COND22 N1956X FUEL STK VT VLV CLSD23 N1960X F MAIi DRN VLV CLSD24 N1961X F YAIN DRN VLV OPEN45 P1988X MSL LC2 9 95%57 N1951X PRESS DuCT FUEL SNSR58 N1962X LN2 VET /LV OPEN59 N1963X L '.*'4 DRN VLv CLSD60 N1964X L tAi'i DRN VLV OPEN68 F1897X FLIGHT HE 1 VLV CLSD69 N1892X L.2 LOAD VLV CLSD70 N1893X LN2 LOAD VLV OPN71 N1894X LN2 STK P VLV CLSD72 N1895X LN2 STK VEN T VLV NCL

2. THESE PENS DEACTIVATED THRO5GHOUT THE TEST

5 P1997X MSL FUELED 95%25 N1965X FUL DRAIN COMPLETE28 N1970X AA cUEL 95% PROBE30 N1972X AA FUEL 99989% PROE32 N1974X HW L02 BU 95% SIG35 N1977X HW L22 TOPG COF SiG36 N1976X HW L02 EM S G 1i0.2%39 P1892X R. ROBE T STA 79374 P1894X LC2 95% EMERG COF

This document' ntams information afhectng the natonai defense of the Un,ted States vthn the meaning of the Esp'onage Laws Ttle 18

USC Sect'ons '93 and 734 The tansmss,nl o' thp '(,elatlon o' Is contents ,n any rannpr to an ,nauthorzed person is poh b,ted by Il

SA 7022 CN-F--NT I A L

Page 37: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

CO*NFiHfNM AL ____~

CONVAIR ASTRONAUTICS u ____

Instrumentation Survq

Instruma~tion nafunzction.92 causes and c~rrective ac~tions are shm inthe folloving table.

This document zontains informTation dffctng th natonal defers of t~e Ur ted State: ,t n the mreaning of the fsponage Laws Tttle 18USC Sect ons 793 and ;9. T~e transmss o, or t5, reveatior oft content r, any ranne o an unau! orjzed peson i, p~ohibited by law

PV~ A 702 2--NFf- - --~ .

Page 38: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

CONVAIR AST"RONAUTICS put ____

o ILL.

C7

"i ~j j -~-a-W f -I foililt tw efneo h W W ltiwti hem W fteEp2 as il 8US1 , 4K~ 9 W74 MtIMM III1 fIICN141 4M e 4"M O~dpo soli ylw

M I-fM A

Page 39: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

~~CO N FIEN-TEALr.EPORT v 1299

CONVAIR ASTRONAUTICS E-

INSTRUMENTATION FAILURE CODE

1,TRANSDUCER Es 400 CPS DISTURBANCEF. NO USEABLE TIMING

A* DAMAGED BEFORE TEST Go NO SPEED LOCK-USEDB. DAMAGED DURING TEST EXTEQ',AL SPEED LOCKCo POWER SUPPLY LOSS H. NO i,'5ABLE 100 KCDo EXCESSIVE ZERO SHIF7 IN CORRTCTION

INSTRUMENTATION SYSTEM I@ 'O ',- AtLE VOICEEs EXCESSIVE GAIN CHANGE IN Jo AONG TAPE SPEED

INSTRUMENTATION SYSTEM K. FAULTY TAPEFe OPEN CIRCUITGo WATER IN TRANSDUCER 5*TELEM'ETRY /NOT APPLICABLE/He SHORTEDI* EXCESSIVE RANDOM NOISE 6*PRE-TEST MEASUREMENT CALIBRATION

2.GRAPHIC RECORDER A. NEVER CALIBRATEDB. NC CUEABLE ZERO LEVEL

A. DATA PEN NOT WRITING Co NO USEABLE SENSE STEPSB. TIMING PEN NOT WRITING D. CAi.!:RATiON NOT RECEiVEDCo PAPER DRIVE STOPPAGE FROM TE$1 SITEDo RAN OUT OF PAPER DURING E. CALIBRATION SUSPECTED TO BE

TEST INVAIADE6 EXCESSIVE RANDOM NOISEFe NO TIMING 7*INSTRUMENTATION PROCEDUREGo OFF SCALEHe PAPER DRIVE ON SLOW SPEED A. WIRING REVERSED

B, CA''BR4TION RANGE INADEQUATE3*OSCILLOGRAPHIC C. SYSTEM SENSIT:vITY TOO HIGH

Do SYSTEM SENSiTIVITv TOO LOWA. EXCESSIVE RANDOM NOISE E. IMPCSSIBLE TO MAKE MEASURE-B. BAD GALVANOMETER MENTCo NO TIMING LINES F. MEASUREMENT NOT ATTEMPTEDDo NO TRACE IDENTIFIERS Go IMPROPER WIRING CONNECT:O"Es GALVANOMETER NOT SUITABLEF. RAN OUT OF PAPER DURING 8@MISCELLANY

TESTGo PAPER DRIVE FAILURE A* RECORD DAMAGED AT TEST SITEH. NO TIMING CORRELATION Be RECORD DAMAGED IN TEG

Co RECORD NOT SENT TO TEG4.MAGNETIC TAPE RECORDERS Do RECORD LOST IN TEG

Eo RECORD NOT IDENTIFIED AT SITEA. SIGNAL OUT OF BAND F. OSCILLOGRAPH DEVELOPMENTB. EXCESSIVE SIGNAL DROPOUT FAULTYC. EXCESSIVE RANDOM NOISE Go TRANSDUCER NOT MOUNTEDDo 60 CPS DISTURBANCE PROPERLY

He TRANSDUCER MNTD AT WRONG PLACE

7his document contains information affecting the nation3l defense of the United States within the meaning of the Eopc:nage Laws, Tit!e 18,

Us Sections 793 and 194 7he transmission or the ievelaton of it contents in any manner to an unauthorized person is r nhibited by law

A 1022 AO-N-FID 1A L

Page 40: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

C Of--T-IA L Addenrdaomv IM 12 99)_

CONVAIR ASTRONAUTICS PAer 35

APPENDIX 1

~Tables an Figures

j

This document contains information affecting the national defense of the United States within the meaning of the Espior,age Laws, Title 18,USC, Secions 793 and 794 The transmission or the revelation of its contents in any manner to an unauthorized person is prohibited by la v

FORM NO A 702? E" A L

IOM ,, r EI A

Page 41: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

~~~CONFltDENTIALt,,,,,

CONVAIR ASTRONAUTICS PAu 3 6

TABLE 1

02 Sample Data

Ran 423

.Noe Tank lN2*

T - Tanking

2 T-30 32 18.6 99.3 .74 T-80 28 28.0 98.1 1.91 D-95 12 44.6 99.1 .9

D-80 9 66.9 99.0 1.06 D-60 11 51.1 99.4 .67 D-40 10 42.9 99.3 .78 D-20 8 66,2 90.0 1.03*

* Sample number 3 was inoperative for this run.*i% 02 and N2 are shown iL % of remaining sample after HE is removed.

L02 Storage Tank Sample, %02 %N2

Before Run 423 99.4 .6After Run 423 99.8 .2

Run 424

Sample No. % Tank Level Press. % HE % 02** % N2**

T - Taning

1 T-30 30 14.8 99.3 .72 T-80 20 29.2 98.7 1.35 D-95 11 55.9 99.4 .66 D-80 14 44.o 99.3 .77 D-60 12 44.3 99.4 .68 D-40 12 46.8 984 1.64 I20 9 51.8 99.3 .73*

* Sample namber 3 wain noperative for this run.*s% 02 and N2 are shown in % of remaining sample after HE is removed.

This document contains niormation aftecting the national defense of tne Unite" States withi,, the meaning of te Espionage Laws, Title 18,USC, Sect,ons 793 and 794 The '.nsmission or the revelation of its contents in any manner to an unauthorized person is prohibited by law

I FYNMo) A 7022 C-nf+Ht3Nft

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Addend=I1

CONVAIR ASTRONAUTICS pur 37

TARLE 1 (Continued)

I.02 Storage Tank Salple: % 02 % N2

Before Run 424 99.7 .3After Rum 424 99.8 *2

PPeN* % Tank Xevel Preas. %IM % 02** %N124*

T -Tankg

1 T-30 30 22.1 99.4 .6J2 T-80 30 23.1 99.1 .9

5 D-95 27 32.1 99.2 .86 D-80 30 21.1 99.5 .57 D-60 34 21.2 99.2 .88 D-40 37 30.3 99.2 .84 D-20 32 22,4 98.9 i.13*

* Sample mmber 3 was inoperative for this run.*4 02 and N2 are shown in % of remaining sampe after HE is removed.

L02 Storage Tank Samples % 02 % N2

Before Run 425 99.8 .2After Run 425 99.7 .3

This document contains information affecting the national defense of the United States within the meaning of the Espionage Laws, Title 18.USC. Sections 793 and 794 The transm'ssion or the revelation of ifs contents in any manner to an unauthorized perso, is prohibited by law

loRY NO A 7022 LN1 ENTAL

Page 43: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

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Page 44: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

CO ID-E -fAt Addendum

EWU_ P! 1299

CONVAIR ASTRONAUTICS pm 39

TAMLE3

Fuel Tank Temperature Data

Fuel Tank HeliumF1004T

Test No. Pre Test Max DGF Amb Temo DGF Acoustica PerformanceDGF 0 Time in Mir.

417 104 132 @ 3.0 92 Satisfactory

418 122 *150 @ 3.0 106 Satisfactory

419 105 146 0 2.3 100.5 Satisfactory

420 105 *150 @ 3.0 P8 Fuel 95% probe failed

421 108 *150 @ 2.0 94 Satisfactory

422 120 *150 1 1.4 104 Satisfactory

423 99 145 @ 2.3 93 Fuel 90% probe failed

424 114 *150 @ 1.7 92 Satisfactory

425 120 *150 @ 2.0 100 L02 90% probe failed

426 128 *150 @ 2.6 102 Satisfactory

* The range of this recorder does not exceed 150 DGF so these temperaturesare higher than the systez is capable of measuring.

This document contains information affecting the national defense of the United States within the meaning of the Espionage Laws, Title 18,USC, Sections 793 and 794 The transmission or the revelation of its contents i anir manner to an unauthorized person is prohibited by law

FORM No A 702 2 6-O-fnJ- nuUEJiIA L

Page 45: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

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FORM NO A 702 2 D RL

Page 46: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

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FORM NO A-702F2I-Dt-tfA L

Page 48: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

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Page 49: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

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Page 52: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

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Page 54: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

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i ORM NO A 702.2

Page 56: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

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Page 57: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

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Page 58: TOculator In temperature (PI925,") rose above -291 DO? at 11.5 minutes and re-mined warmer than this temperature until 17.6 minutes. See graphic presentation for details on L02 Recirculator

CO FfB-NfThAt end

CONVAIR ASTRONAUTICS PFa3'

APPENDIX 2

Operating Conditions

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This document contains information affecting the national defense of the United States within the meaning of the Espionage Laws, Title 18,USC Sections 793 and 794 The transmissoir " the revelation of its contents in any manner to an unauthorized person is prohibited by law

FORM NO A7022 0 Nff9-! W J A L

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CONFiDtN"iAL _

CONVAIR ASTRONAUTICS P IL

RE LINE VAIM EXCEED)

No red line values were exceeded during Runs 423, 42, 425 and 426 . Redline values are tabulated in Test Directive ETD-O] -5,

This document contains information affecting the natonal defense of the United States within the meaning of the Espionage Laws, Title 18,

USC, Sections 793 and 794 The transmission or the revelation of its contents in arty manner to an unauthorized person is prohibited by law

FORM NO A 702 2