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NASA TECH N ICAL NASA TM X-71521 MEMORANDUM (NASA-TM-X-71521) SECOND HEATED JETTISON N74-2054 TEST ON THE CENTAUR STANDARD SHROUD (NASA) 110 F HC $8.50 CSCL 22B Unclas G3/31 34366 , WIt 1i February 1974 February 1974 https://ntrs.nasa.gov/search.jsp?R=19740012431 2020-07-05T07:00:27+00:00Z
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NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

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Page 1: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

NASA TECH N ICAL NASA TM X-71521MEMORANDUM

(NASA-TM-X-71521) SECOND HEATED JETTISON N74-2054TEST ON THE CENTAUR STANDARD SHROUD(NASA) 110 F HC $8.50 CSCL 22B

UnclasG3/31 34366

, WIt 1i

February 1974February 1974

https://ntrs.nasa.gov/search.jsp?R=19740012431 2020-07-05T07:00:27+00:00Z

Page 2: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SECOND HEATED JETTISON TEST ON THE CENTAUR STANDARD SHROUD

Lewis Research Center

National Aeronautics and Space AdministrationCleveland, Ohio

ABSTRACT

The second in a planned series of heated jettison tests onthe Centaur Standard Shroud was conducted at NASA Plum BrookStation's Space Power Facility on January 16, 1974. Thefirst 250-second portion of the test sequence involved heat-ing the shroud with a specially-built fixture designed toprovide a simulation of the heating environment encounteredby the shroud during its ascent through the earth's atmos-phere. The two heater halves, which were mounted on a railsystem, were then retracted. This was followed by the jet-tison of the two shroud halves into catch nets positionedat 900 to the heater rails. The condition which made thistest unique compared to the others in the test series was thealignment of the maximum thermal line with the shroud separ-ation plane. Information on the test hardware, configuration,and sequence is presented. Shroud thermal and deflection data

o encountered during the heating portion of the test sequenceis compared with free-skin design temperatures in variousgraphical formats.

i

Page 3: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

INTRODUCTION

The Centaur Standard Shroud protects the payload of the Titan-Centaurlaunch vehicle during the ascent phase of the flight. To conserve weight,it is jettisoned as early in the flight as possible, while it is still hot

from aerodynamic heating. Analysis of the possible flight trajectories and

the shroud structure indicated that severe internal stresses could be built

up prior to jettison. Calculations of the edge motion of the shroud duringjettison indicated that the design clearance between the shroud and the pay-

load could disappear, in the worst case.

An experimental program was conducted in the Space Power Facility at theNASA Lewis Research Center to verify the computer model of the shroud jettisonevent. The shroud was heated to simulate the expected 280-second flighttrajectory then it was jettisoned.

A seven-megawatt, radiant heater was assembled in the vacuum chamber ofthe Space Power Facility. The heater was programmed to produce the desiredtemperature distribution with the plane of symmetry aligned with the separa-tion plane of the shroud. Fdllowing the 250-second heating cycle the heaterwas pulled away to allow the shroud to be jettisoned. A special catch net

system was built which allowed one half of the shroud to fall completely freecf the launch vehicle while the second half rotated approximately 160 beforebeing caught. The test was performed in a 20-torr environment.

Deflections of the shroud were measured during the heating cycle withstraingages and deflectometers. Thermocouples measured the aprlied thermalcondition. High-speed motion picture cameras were used to record the motionsof the shroud during jettison.

It is the objective of this report to present a brief description of thetest hardware, the operation sequence and the results of a preliminary dataanalysis.

APPARATUS

The overall arrangement of the test hardware in the Space Power Facilityis shown in figure 1. The seven-megawatt heater was built in two halves thatrolled on rails perpendicular tc the facility rail system. The Centaur shroudwas mounted on a Titan-Centaur interstage adapter. Its location in the 100-foot diameter chamber was chosen to allow one half of the shroud to fall com-pletely free of the hinges before being caught in the net. The other half(the one with the dome) was caught after only 160 of rotation. The Centaurtanks were not used in this test because of the unnecessary complexity theywould have added. In their place, a special structure was mounted on the

1

Page 4: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

interstage adapter that allowed access to the inside of the shroud and supportedthe flight truss adapter, equipment module and a simulated pay-load. A photo-graph of the internal structure is shown in figure 2.

Catch Nets. Special catch-nets were constructed using a high temperaturesynthetic webbing supported by 6-inch-diameter aluminum pipe frames. Thephotograph in figure 3 shows the full-jettison catch net in position. The

full jettison net frame was supported by cables attached to 10 disk brakes(five on each side) which served to absorb the energy imparted to that shroudhalf. The catch system was pre-tested using a model of a shroud half to in-sure that it would function properly without damage to the shroud.

Heater. The heater was designed to duplicate, in time and temperature, thecondition expected in the ascent phase of the flight. The heater contained5910 tungsten filament lamps inside a highly polished aluminum reflector. Adetailed thermal analysis (the approach used is described in ref. 1) andextensive small scale tests were performed to verify the design concepts.The heater was divided into 18 separate control zones, 11 in the cylindricalsection and 7 in the biconic section, to provide the proper circumferentialtemperature profiles. In addition the spacing of the lamps was varied withineach zone to control the vertical distribution of heat. Because the desiredtemperature profiles were symmetrical around the maximum heat line, the 18control zones were further divided into mirror-image half-zones (one on eachside of the plane of symmetry). The arrangement of the control and mirrorimage half-zones is shown in figure 4. The maximum heat line for this testwas at an azimuth of 00 (00 from the shroud separation plane).

Control Systems. Each control half-zone and its mirror image was powered bya separate SCR controller. The 18 controllers were programmed individuallyto reproduce the expected temperature vs time curve for their respective con-trol zones. Abort limits were established to insure that the test would notproceed if any control half-zone or mirror image half-zone deviated more thana prescribed amount from its desired temperature curve.

A PDP-8 mini computer was used to conduct the test because of critical timingof events necessary. The sequence of events for this test is presented inTable 1.

INSTRUMENTATION

Thermocouples, straingages, deflectometers, and high-speed motion picturecameras were used to measure the performance of the shroud during the test.Digital data were recorded every second during the test, using an XDS 930 com-puter. FM analog recordings were also obtained of selected parameters. Thecoordinate system used to define the location of sensors on the shroud isshown in figure 5 and 6. The cylindrical section of the Centaur shroud is acomplex structure composed of a corrugated outer skin bonded to a smooth innerskin supported by circumferential "Z" rings. A sketch of the structure anda typical free skin thermocuple installation is shown in figure 7. Free skinthermocouples were located as far from structural masses as possible to pro-vide the best possible measurement of the thermal environment. Free skin ther-

2

Page 5: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

mocouples at station 2626 in the cylindrical part of the shroud, and atstation 2724 in the conic part were used to provide temperature feed backto the power controllers.

RESULTS

The heated jettison test was conducted on January 16, 1974, at anambient pressure of 20 torr. The heater was programmed to produce the de-sired temperature distribution with the plane of symmetry displaced 00from the shroud separation plane (see figure 4). -The light half of theshroud (the one without the dome) was fully jettisoned and fell free of thehinges into the horizontal net. The other half was caught after only 160of rotation.

Time histories of the control thermocouple readings are presented infigure 8 for the 18 control half-zones and the 18 mirror image half-zones.Included also on this figure are the desired temperature histories. Com-parison of desired and measured temperatures shows that excellent agreementwas obtained. The greatest deviation was in zone 10 where a 100 F deviationwas observed in the mirror image half-zone. The instantaneous power appliedto the shroud varies according to the slope of the desired temperature curve.The measured power applied to zone 1 is presented as an illustration in fig-ure 9. The initial peaking power occured because the shroud was cooler thanthe set point when the heating cycle started. The power increased gradually,following the desired temperature curve. Very little power was needed nearthe end of the cycle because the required temperature was actually decreasingslowly.

Circumferential temperature profiles are presented in figure 10 at severalstations and for several times during the heating cycle. Also shown are thedesired temperature profiles. Comparison of the two indicates that very goodagreement was obtained everywhere except at the top of the biconic sectionand at station 2250. The thermocouples at station 2250 are very close to theaft seal bulkhead which probably accounts for their low readings. This is6upported by the fact that a thermocouple at station 2469, where the shroudskin thickness and the lamp spacing were the same as at station 2250, agreedvery well with the desired curve. These deviations were observed early duringthe heater checkout tests and were deemed acceptable.

The shroud deflected during the heating cycle because of temperaturegradients of as much as 900 F in the "Z" rings. The deflection was measuredwith potentiometer type deflectometers. Circumferential plots of theirreadings at several stations and at several times during the test are pre-sented in figure 11. For reference purposes the desired temperature curvesare also included in figure 11. Examination of these data indicated that theshroud assumed a pinched cross section with the narrow part at the shroud sep-aration plane. The tendency for the shroud to pinch this way is resisted bythe joint between the two halves. Consequently, when the shroud is separatedthe first motion is expected to be inward. Edge motions of the shroud wererecorded by high speed motion picture cameras. At the time of this writing,the cameras data had not been fully analyzed and could not be included. How-

3

Page 6: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

ever, it was observed that the first motion of the shroud edges was inward(about 31 inches) toward the payload. In addition to the cameras some shortwooden sticks mounted in foam blocks were installed to indicated invasion ofthe payload envelope by the shroud. First inspection indicated that the pay-load envelope was not invaded.

Examination of the camera data also revealed small objects (tape-likein appearance) being blown off at high velocity from the Super*Zip near thehinge in Quadrant II (at approximately 1000 azimuth).

CONCLUSIONS

A successful heated, jettison test of the Centaur Shroud was performedin the Space Power Facility on January 16, 1974. The shroud was heated tothe desired thermal condition with the axis of symmetry displaced 00 from theseparation plane. Initial observations indicated that the shroud's firstmotion was inward but that it did not invade the payload envelope.

REFERENCE

1. Hemminger, Joseph A.: Computer Simulation of Temperatures on the CentaurStandard Shroud During Heated Jettison Tests. Paper presented at theSeventh Space Simulation Conference, Los Angles, Calif., Nov. 12-14,1973.

Page 7: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

Table 1.SEQUENCE OF EVENTS

Event Test Time

Start all recorders. -10

Verify recorder start. - 8

Start heating cycle. OVerify heaters started. 50 to 80

Color movie lights on. 160

Color cameras on. 165

Safe zone heaters. 250

Start heater retract. 250

Turn on movie lights. 272

Check heater clear. 272

Start cameras. 272 to 275Arm seal pyro. 275Fire seal pyro. 276

Verify seal pyro fired. 277Arm instrument disconnects. 277

Fire instrument disconnects. 278

Verify instrument disconnects fired. 280

Arm Super*Zip for shroud jettison. 280

Fire Super*Zip. 281

Safe all systems. 295

Stop all recorders. 300

5

Page 8: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

Partial JettisonCatchnot Top Structure

- -~-- Towers

Payload Envelope Mcdel

rIo

IOpenChamber Door -

CentaurSimulator

Full JettisonS Catchnet

Figure 1. CSS in jettisoned position (view looking north).

Page 9: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

Figure 2. Photograph of internal structure.

Page 10: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

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Page 11: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

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a; Station 2626.5, loo ing art. (b) Station 2723.45 (15* cone), IcoLnL aft

Figure 4. Heater control zones and control tlhermocouple locations.

Page 12: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

- Sta. 2867.25

Dome Non-dome3hroud Shroud HalfHalf \ Super*-Zip Joint

-- Sta. 2680

Payload Envelope ModelRetractedEncapsulationBulkhead -

Retracted --- Equipment Module

Forward BearingReaction Struts Truss Adapter

.- Sta. 2459.0

Forward Seal - Stub Adapter

Centaur Simulator -- .

SCentaur Standard Shroud

Aft Seal --

- Sta. 2242

Sta. 2209 ,t.a. 2709 Interstage Adapter

Sta. 2127.4

Figure 5. Axial coordinate notation - station locations (inches from datum).

/0

Page 13: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

N

RAtANT HEAER.Du ksiCg Je-TI-saV

o-ll I

* P 0R 20 - -00E

S

+Z

Figure 6. Angular coordinate notation - azimuth (plan view, looking down).

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Page 14: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

Corrugated skin

Smooth skin

Inboard

Note: thermocouple junctions located between"weldbonded" panels spot welds.

Corrugated skin

Smooth skin

L 2a Z-ring supports

S 2a --

Typical mounting on cylindrical section

Figure 7. Free-skin thermocouple locations.

/)

Page 15: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

Figures 8.1 thru 8.36.

Design temperature and thermocouple historiesat heating zone control locations on CSS.

T

Page 16: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

'.; I:;T RUIN 48. 0 D1. SI lI HEI LE: ..TT ISOM TIME DRY HR MI SEC VMILLPLOT Htril R 06 1 IlNE VS TEll" ZOIIE 01 FST. PT.016 13 1 10 8537 Figure 8.1

2 (727T) 4 (011T) 5 (Design) (012T)

)..i 50. 000 0o0.00 150.3 200.00 250.00 300. 00 350.00 4 00. 450. 10510 .00 :--I-I I II I I I-- I t :- 1 II-I I I-1--II Z I I- - I- L : I I tFI-I I "[ f-I 1- l-I -- -I- Il - I1 I I-1 1 1 1 I-I--I--I-I --I -- I - I I - 5 0.

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Time seon--F d

5 Design Temperature6 Data Thermocouple

-LF1 t 1 1 1 i I I I I I i I - i- ii

.0: -_1 nf I000 :; I m0- ::::I 00 300)0 11 4 1 'IPU W1 .00

Time (seconds)

Page 17: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

'.iF CU T RUN CS 0 DI.G : Il -! . I Il (IE I' IY I: i:i S I Il IPi 10T 1 : R [18 I l: VS T:L' CONE 81 FS I. PI .!: 16 13 I 10 F gure 8.2

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Dimp Tmerntue l

Page 18: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

F L - .T RUN 4., DIG ' -tI i HEIF JITr IISC H TIME D:'Y1 HR 11111 SEC MIII.L

PIo 41.i::IR 14 l I; VS IEIINS'- NE 12 FST. PTI.016 13 10 10 ,57 Figure 8.3

A (728T) c (016T) r,(Design) E(017T)

. -.. 030 100. 150 20 , 20. 2J. ' 2 30 00 350 08 400. 0 450 . 08

500. -I : : ! - I 0: 1-li : H I i I l l - I -1 1 1 -- H -- I: I i -! -+- I 1 1 I- 500.08

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Time (seconds)

Page 19: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

,'IF C.'T I::T RUIJ 48. 0 DEG SI:I HlE(I D Li II1[ISON TIMFE DY FIR MIII SEC MitL.FPLO.UT .;;;: R 16 1 l1. VS 1i1I*P- DONE 02 FST. PT.016 13 IE1 10 857 Figure 8.4

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F

Mirror Half-ZoneF Design Temperature

- 800. 013 "I-- I-I I- i i-I --- IF -t - l I Data her ocouple +4- l-- - -I-l tI -I-1 I-- -- --lI -- I---+ I-I I-I I -48.8

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Time (seconds)

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Tie(ecns

Page 20: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

aIa . ;:.T ' U , 0 - Sa I . I ' .1:11 !:N 1 H IlF I:.Y HIR IIH:I SIEC Mill.

R 1 I. 11,. VS I 1J -"II0 1 FS .L'1.1 13 11 10 8 ::?, Figure 8.5

2 (729T) 4 (021T) 5 (Design) c (022T)

v. : 000 - . 0 ; 200 . . 00 200. O( 350. 00 4). 00 4'0. 00buo. - I I I - I- I 1 1 , I i .

0 0 . I i i 1- I --1 - -I I--I- 1 I -H - : I--I- I 1 ,

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' :". ! .; 4 Control Thermocouple - 'tO , ' ' I , '1 .

Data ahermocouia a

W1 f± 1 110

Ti4... I nnriI

Page 21: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

;rF CuS ';!T RLIN .1:, 0 DEG SKI! I-Il l F i I ' 13l._ 1 1$. !:o Y FIR i1! 'S:C I II

PlOT 11I R 08 li VS 11tI-' .- ONE FS I. P1.,16 13 1Ii 10 8u Figure 8.6

7 (Design) a (017T)

S00 100. 0O 00 300O. .- PZ. 00 0 40. , 41.i. 00

500.CO Ei l I ! I :i :I I 1 ' SI I I

408. 00 - I A 1 1 1 I i I f- I 1 - 400. 00I 4:

7 -

7

7

O 1000.II -II- I -+-II - II -+-if - 4-1 I -1 I II 1- . 00

Mirror Half-Zone

7 Design Temperature--. 00.; I- .- I-? : 8 Data Therm Ocouple :-: : - I : I -

201.. 1 1 I- " I -' , , " 1 | i , I- I I 1111 !- I I -j I- I I I tI: I I I ; ! 1

.'': 1 00 (1 - , "O (se2co- . 'ds:.0 300 . 1 b? i .Time (seconds)

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'I L .' I LIN . 0 1 fhi 11 F I .I I I J1 IM I IIIE f:Y IR II I SI-C III I-

Lor HUFI.. R 141 Ill' VS ILi - OE 034 . FST. PIJ.016 13 10 10 8b' Figure 8.7

A (730T) c (026T) B (Design) E(027T)

':. . 0003 100.00 1.5000 200. f; 2--i 00 .300.00 O 50. 00 400r 00 4! '. 00

400.0 0 1- 1I I- 1- 1 1 -I-I --1 ~ 1 I-- I I - - I--t 1 1 -l--- --- I I -- --I-I-- -I--t I -- I--I- : I

300.00 i +--IFI-i- -F--1 F I - F I4 1 -+ t 1 1 VHH 1 F- t r (-

SI I 1 - -I 0

00. 00 ---- -tI-I ---II t-l l---I--I- - -I F -H - ------I--t

H--l---- I----l- t--+-----i'I - i

E- 200 I I F--1 -- I { I I - -+ -1f-1+I- -1-- 1 1 -I-- 1 + +Y . 0

Control Half-Zone-,.,o -: :-- : A Programmer Signal Temperature I -- I -

-too.CIO -1-- +--II- i -1 1- 1- -I -I I -I 1-I I + HIIIff 1I 1_1 f-+ I--If I 1_4 1 _f_ f 4-

Time (seconds)Time (seconds)

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1: U'_< '-IsT RUN ,18, 0 DFG 'FI I -II11.11 .JIJ IUSON TIME DPY HR fliI SEC Mill_PLOT NU:LR 16 fll!E VS I O;N:' ZONE 04 FST. PT.ol16 13 10 10 85? Figre 8.8

F(Design) a (102T)

.. 0 , 50 000 1 0. 00 150. 00 200. 00 250. 0088 300. 0 350. 80 400. 0 450.00

5 C0, 1, :--A I III I- i ,, I- A 1 ; 1- I-+ - l - I H 1 - -- i-i 1----II -- I I I i i H -I - A - I- 1- -- I I --

5 00 .00

400. 03 1- 1 1 1 I I 1 4- I A I I--1-- I I - 1 - --+ -1 - - I- - H -l+ 1 -l--I I I- --1- 1- F - I Ii. I-+ I -f I I I - 1-4 i -I 400. 00

G G

V ~300.00 ++) + - -4ElI- I -I--+ I 1 +I t 300.00

20000.00 i-f-I- -F -1 - I-- I -- - +---i--I I + ---I---+- - -- -+-F-- --- I-I- - -It -I--H -- I I+ 200. B8

FFF

100. Be 1 + -4-I- -1---I-1- 4 1- I I -- 1---- f -- ---- i -- tI-+--i-+-+++- - -f--+-- t

-+ + 1i 1+ - 100. 08

aFFfFiffi f fi-t FF FFi-FffI C C I t~.00000 I---i F l- F -I I- I -I-I--I-I I--F- - -- I-I -l- -- I - H I-I H -- i -I--i -I- ---f -+-- ----I- + -- -- -+ - -1- F - -I I I-H-- - 1-- t I- .00000

Mirror Half-Zone

-lFeI0 -- II I I : F Design Temperature I-- I I ---- -F- I F I H: -- -1 i o.000 Data Thermocouple

S. .- -I i - I : i - ,I I 1- i - I I II I --I I : I -I I + I i --I I I I I | I I -2 s . u

lc ± 0. 00 150. 00 24 . 0 2:.08 30. 00 3502. 10 4'0 im so. 00Time (seconds)

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S L:; '. T IUHfl .1 , D, G St 1 U Il l. 1 ri I-;N It IME 1I:Y IR 111 S1 C Ili .

I .;1 R 06 I r., \VS lI;' O, W- FST. PIT.116 13 Iii 10 E85 Figure 8.9

2 (731T) 4 (031T) s5(Design) 6(032T)

"t :. 1 ~I 0. 15, O.- 200. 00 25. 0 300. 00 350 0 4 '0. TU. 0

530 e , -I I - i- -il I I H I I i i I I I I -1 1 1 1-1 -1 1 i 1 - 500.00

400 - -8.- - I 1-+ 1 I I -+ - II - - i 4---F 1 -I I i -+ -I -I II - - 400. O

200. 3 I -I I II 1 I-, I - 1i -I -I I -I F I I 11-- I-I ---II- I I 1 I I 300.0

SIL200. 04 III I I -1 i1 I-V - 2300. 00

55

5

1. . . . .I ,- I - 1- I I A-- t 1t I- 1 e O

[.0!. ! I ! I I f- .1- I - -I-- -I I-I I- I--- I-I1 - ,- I - .-

2 Programmer Signal Temperature

to I- I i : I i I : : I-I I I 4 Control Thermocouple I- :- -oo.0o

5 Design Temperature6 Data Thermocouple

- 1r; 11 i o I l 0i 21, !1 . 300 d3 3-i 1- 1 .I G.3

Time (seconds)

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'l;- C- i 1 RUH . 0 in ; .1 H I 1 I SON TIM E I l: Y [lR [11H SE:C 111 I

Pi 01 H- :R lS ISll VS I-, .'ONE f15 FIT. PI.116 13 10C 10 8'jc Figure 8.107 (Design) a (097T)

it Jt3 1310 15 >0 20 0 2-. 00 300 00 2 8 0 O.v '.00I I! - I

S! i I - 40.9 f i l 0

, --fq_ 1 - I 1-1 1 -1 ; I II I- - I I -I 1- ! I - I I +: J- I c , - o I +

4)

7 -

7 7

i0. 00 I- l I - -I - i i I -I-- I I I-i I I A l. - + - F 11-+ + 1 i - - I 1 -- f I I I -I 100.00. 0 - -I F i I t- II - I -Ii I I --I --I-I I - i- I1 - I- I -- -t- I - - I i-+-H I 1-I H. -I i i .

iO-i.g -T ptI F- + I I I IF I- 1-I I- I -I--F F:A I-II- I 00.

8 Data Thermocouple

-: -I : I I I I- . FtI H I I -- I I-,I I -I- II - ---I I -I-l-- I - F-F I- -I I I I i-I ! -I I I : - . r- 88.0i

T so

1@1 r1 o 150- 2'':,- 00 30000 3t o i' .,')

Time (seconds)

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L: , C ' . I_,T RU -IN .2 3 8 lI i- 1 nl i 11l I III i N I iE PIY K11. llI SIC tII l I

i II :;, R 14 '1I 1: VS 11M11' ONE ic. - FST. PI. F16 13 10 10 857 Figure 8.3.

A(732T) c(036T) D(Design) E (037T)

0 0 100.00 110. 0 I 200. 00 50 00 300. 008 350. 00 402'. 10 450.010

50 l3 I-I I I I I - -I it I I +- i I - I I I-l I I ---II -l H I -- - lI I- 1- I I-I- :I -+ 1 I -I F I I 1- .300 130

I4I

08. 8 ---I-- I ---- :- I --- I --I-I -l" -' - ' --I---I I: -l---I---I- • I-t ,-I--l ---I I--F--I--I- -I--I . -l----F-- ---l--- -I----- ------- I - --- I-l-- l-I--I--I-- 88.

-200.110 .- I -I+ lI .1 - + H- -1F-iI -l-1- --I --- - I---I-I- - -I-l-l------I--- 200.00

II

200.00B1 -- 1 - I- +- -1- - -1- I- -iA Al i-lf II -1 --1 -" 11 -1 - Fill H H I--F- " -1- I-I-1- - 200.00

nI

00. 3 -- H--l--A -- I---I It +- i I -f I I I- --- ~ l' 1- AII----- ---'--- - I-I--I -- - - I-- - -- -I-I- - 00.00

sA A A Atn

Control Half-Zone

-o. , r --- : - I - I + f A Programmer Signal Temperature H-+-- -I-- I I-H-----I I H--I I 1 -H-. - 1 I H -310C Control ThermocoupleD Design TemperatureE Data Thermocouple

H. l I I I I I I I -I- I I - I I I -I I- I- - I I I I I I- - ,A.i 6. .

11.00 10 U. riM 156 CI 2o 00::J. DO 330030.0 fie350.0 e i'll 4'-, 00

Time (seconds)

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(spuooas) OurT 00

0o i;i- o. .0 on n 000o 00 P ilou c0 0 i00 coI U§ .

I i I A 1 1 fi I -I 1 I i I II I I III

-I--F IF----+F-I -I - -+ednooo 1 Hot a 0I-eI I I00"OOT- -- I--I I -F - 1-+I --I- I -I-I---I I I---- -I I I-I A -II

eGoZ-TeH oJZ{I

S +-.I- I I .1--+- -I -+-- --4-+ --- I -- --I --- ---------f-l- -- --- I-I-- I 1I--I--I o

_-AAA

4o -----I- -- 1- H- -1-1 1 4-1- I --1 -- -I -I---H 000

000 -1 4-ttl 1F + -F--4l; F--lI- I -- 1- -1- 4-1 I1--+ I I---iF4---- I-I -I-I--I 0 0132I

0080k 1 f -I- --tH ------I- I I-I- 4- --I LI- I FA-l I-I-I I -H 1 -411 H 1 1- -1 1-1 F -I-I-lH -0 0'U

o I ,Nr I I I I-I I I .1-I I 1-+ 1-1 I I I- -1 I I I 1 I -I I I I I I I i -I I I -I I I 1 I I 1 00

OO3 0 080017 go 00 2 00 0 oS 002. 0' 01) o "0 00 001 000 '0 -"

(uZ60) (uSaS))

u't e.uriT 2.98 01 01 LI 91 '.lId lS J 90 3H02-,It-il SA :1-Il L 91 d ':i!tI .0l7-4

II11W 33 NIW H Ur -1W,111 O1"lII- U-LUH 9EI 0 'p M ; 1 :1 A.1,

Page 28: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

:' C', L: T RIJM 18, 0 DEG SIltJ HEIFlD JEilTlISON TIME DIY HR MI1 SEC MII LPLOT NI" R 06 TriE VS iEMPl-ZONE 07 FST. PT.016 13 10 10 857 Figure 8.13

2 (733T) 4 (041T) 5 (Design) 6 (042T)

' 50 000 100 00 3-5. 020 2 - *0 30002 . 00 00. 50. 00 40 0. 0 450. 004:0 0 1- 1 1- 1 I I I I-I I- I I f-- I I-- -1 1-1 I I I-+ -- I -1 - I I-I f-1 1 I f f 5 .0000

400 0- -I--I- I-fI I I I-I I I.I II-I-I I I I I F- I I I i - - I-I--I -I I I-I - I I -II-i--- f -f-I--I--I I - -. } f-- I--I---- I I -F-fI-l f f I- I-I- lItI 400.00

308.00 -I-- I -I- I ---f--I -I- -- - ' I- + I I I I- II-iIl I---I- I--+ F- I--f- ----- I--I--I-

I-I--I--- -,-I I- I-I- - -I-- - F-l - -- I-- I---I-----I - I-J -I - -- f--I--F- . 20 .30

300. 00 A I- I 4- A + -- t -+ -- 2 0 0-foci IA , + I A4-I F I+_I__: f-1- ' -f--f--f-+ -1--- i - 1 t4

5 5

00000 - -+- I - ---I f- I - --- -- - I I--- -- -I-- -- ' I -i- ' f- L - -I-- -1

1- 21- 00000

Control Half-Zone

01-0 + i- II-- - I 2 Programmer Signal Temperature I.00,0 : - 1 F_- tI I fi t- - f- +--I- I -I- -I -II- - -I I -- '- :I-- - 00

4 Control Thermocouple I I I

5 Design Temperature6 Data Thermocouple

-2f'J-r0 C-f f I - tI I F-I 1- I I I I I I If I I-I I i I I f - I -I .I' - iC0 -i 0 g V50 00 w' '.0-i e s o0s 30 '0.00 3 ' 0 -

Time (seconds)

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; 1'F C, I :sT PUN 48, O DEG SIJ tL HERED J.IT1 ISON I IME DfY HR NIH SEC ill I.PLOT N lti:FR 0B TlMiE VS iEMP ZONE 07 FST. PlT.l16 13 10 16 857 Figure 8.14

7 (Design) 8 (087T)

0 10 50.000 100.00 150.00 200. 00 250.00 30008 350.800 400.08 450.80

500.u. -I + 1- 1 iI I -+ I t++- ,-I -- --- I-I H "I-I I 1-fI-f-1l "- I-- - I II II-t - ' -- I - I-I II- I I - -- l--I- I -I I I I - 500.0

400.00 - --1---- 1- F I - + I----H--+--I- I4--I + 4-4+- -+ -++ 1 1---- +-+ - -+ + -- 400.00

0

3.00. 00 I----I--I-- I -I- -- -- + I---I--- - - I -- -- I-I-H - +---f- --- - -1-,---- -I - -- -H- -+-- -- 4-- - -+--H -4 300.00

E--I

200.00 +--I-I--+ + -- I- ---t-I-- F- I--+--1-i ---+----I- I - F-- --- f-+I -+ +f-I- - 1 - +f- I- 1 -+-t-- I-- -I-- + --I--1- 200.00

7

00. 00 8 8 8-- l i -F -I-! -I-- - -- - -+--+I- 1 -I- 10000

800003 -H--+1- I -I 11 1- -1- , I If --- I-- - I -- I--- ++ 1 - H- F-t-1----+-I-I--I *- I-f-- -H- +---1--4 -1- 1- .00000

Mirror Half-Zone-1.000 -H--I- -I-I- t -- I I-I II - i 7 DeOSign Temporature - --- I I------t--- - -I--I--I

8 Data Thermocouple

-I00.I: I-1I1-I- I I I - I I i-I-I I i I- I 1-I I I I I III- [ I- 1 I 1 I I- I- I -III I-I- I II I I -200 00

. . r; 000 10. 0 i0 00 21+0. no 250. 00 300.00 350 O 4 . 0 4150.Y00

Time (seconds)

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:;' I- C ST RU 4 . 0 DEG SKFI HE-ILD JI I ISCIN T IME DIY HFR 1"III SEC Ht1 I.

FPl-tr HI.U :. R 14 TlItl VS TEII--ZONE 09 FST. PT.016 13 10 10 85e Figure 8.15

A(734T) c(046T) D (Design) E (047T)

- . 5 000 100.08 150. 00 2C0. 0'11 20. 00 00 300. M3 350.00 400. Q 450. 00

500 :- I I i -I -i I-- I I I - - I-' I- I I--I I - I I - I --I I I -- 500.00

4 i I i- i i I1 I - 400.00

200.0 0 --- I I I- I -I - I .F- 4-I IAI I-- 1- fi - +I - 1 - -I I--I--FI h1I-H-+-41

-4-1 --- H tF- , -i - + -I- I - i- 208. 00

D

A A A A--

- I I -I- - - - - I- I--I--I-I -'-I - I I 1 I-

. 0 0

Control Half-ZoneA Programmer Signal Temperature

I23aemo i-: -I --1I l 1 1 C Control Thermocouple I- -

I t" I t I i- -1o3n.0

D Design TemperatureE Data Thermocouple

• .. o- ; - I I 2I II u 00 -00 I "I 300. I0 - I .-51 1 - 1- I -00

Time (seconds)-

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i: :,, I',r RUN .1,. 0 DE G SK[.th HERI L) Ji- 1ISON TIME .AY HR 11N1 SEC IIL I.PI 0 l i :R 16 11T,- VS 1EII ZOE 08 FST. PI.16 13 10 10 85' Figure 8.16

r(Design) c (082T)

C, :3 f3. 000 100.00 150.00 200.00 20.. 00 30008 35 .00 480.00 450. 08500. CO - I i -f 4 - 1 1 1 I !-I- I 1 1 ++t -1 1- I 1- 1-- 1-11 I -++- 1 I + 1 : :- H -1( 1 14 - + 1 500.00

4,0. vO I- I IA H -1- -4 1 + -I--- 1- - +- - - + -+- 1 + f-- -0+ I + + . 1+-I -1 I 1 1- 400.00

300.00 F--l I -I-1 i + - F- - I I-- - -I-- - -1- - t +F-I-H ++ ---- l- - - ---- +-- -H - -++ -IH-+ I {+ I--l--1 1 1- .380. s0

- 200.00 - -H--!- -Fl 4-I-f - I '+1--H+-F++ ---H-F -4- -+ -+--++ +-H - 280.0

FF

F

1 0 0 . 0 0 1- + . I - F F + - - + I-4 - + t + - 1 8 6. 0 0

F! FFF -FF 1 FF0 F F

00000 + -HF I-I +--I-- -+1-F--- I-I-H--I -H---H-+-I+ -- I--H-HF---t -F---+--I- --- I -l--+- H-H -I-41- -i-I-I--I+-- !-H-- -I---I-I-+-+--H-+

Mirror Half-ZoneS-1 - +- F Denign Temperature I 0 1-.--1 1-.V-F++ -F - + H-±-1-1 I -- -100.80G Data Thernocouple L

-200 0 (- I I I I 1 I I I I - -I-I 1 - -1- 1 1 i - I I 1 -i-r o H IZ-n - -I- -1 1 I -I - f I - l--- I I I -I I I I I I - 8a. 00-- ~0.000 10. 00 15. 0 2000 2 .00 300.00 350. 0 400.nO 1.0. 00

Time (seconds)

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S'F :SS IT RUN 4 , O DEG SM-EI I- EAIDI. JFTTISON TIME hiY HR HIN SFC I ll.

PFLO N- HUiWR 06 TIIE VS E IIO-'--ZOE 09 FST. PT.B16 13 10 10 857 Figure 8.17

2 (735T) 4 (051OT) 5 (Design) 6(052T)

t30 5 0018 100.00 150. 00 200000 .00 300. 08 350.00 400. l 450. 0

5'00 0 - -I- I : :- I I +- I F -I I--I- I II - It I ---t- I I I I - -I I .1-1 I - I -I-- I - 5 00.00

400. 0 - --- II I -i -II-I 4- 4-4 I I -I- -+ I- +H --- H - iI- -F--- 1 - -I -- I--I- -- I- - -F- I I ---+++ - 4- 1I- 400.08

200.00 -4---I-1 i 4 ++ 1-- I-A-I+--- I- -- -± -+ -I -4 i - 200.00

5

200. CI +__I-_1-1 1-4 1 + 1 1. 1 4-4 I-"-H -- -1 I-A--A--- --- -...... -Ii- I H--+- I I+ ------ I- --- I- --I-+ -F - -iI-'++1-4--1-1--- 2W 0

10n00 tH- H I -- Id I +$ I Hp I f fH - +---- -- --1 t HA I I 1 o. 10000

08. B I ---l-- I I- - I- -l----4l- Control -I-I -- -- I-i+--I-- +-+- +- -- t- - -i I-- 00 8

-Io. B -- - -- 4 Control hermocouple - I. I : 1-- -100.00

5 Design Temperature6 Data Thermocouple

-2'0t 0 H I--t I I :---1 t :I I I I , , , , I I I I I t. I-I I I I I I If I I I I I -l- -t -- l -I- I I - I I I I I -200 :- 1 "

S- (s 50.e13 I . C10 O. 20n.1 0 .00 3 0, 00 35c. Or I f,- ,11. 3Time (seconds)

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lIF C':. I'1 RIUN 483. 0 DEG SEt!. I 1HE tIED 11- I ISON TIME DfiY FIR MIH SC MillIF'.C1 ll.; :. R 08 TI f: VS TEP'-ZONE 09 - FST. P1.016 13 .I 10 85/ Figure 8.18

7 (Design) a(077T)

. 90 'n. 0300 100. 00 150.00 20. . (10 00 300.00 350. 00 405 3 ' 4.100.

50 0 i- I I i - -I I- I f -- 1 - I I H -I I f1 F-f - 1- I i -- I- I 1 1 1 -4-I I I f I-- -I -1 I- 50 3

400.00 --I--- I I- I I - -I--l-I- -F- -I- - I ---- i I -I--I-f--I-- ---- -F -i --I - - i-f I -- l-H --I + - 1 +-I----I I--[-I 43 0 0

200.08 V -- I 1- - -+ i --I A4 1- t + -+-++ -HI -- + 1- i I.-V - +-1 F-+-+- 11 -++ 1 F- 1 .0

7

7

E -2A0.CA - 1 1-11 I -- 4 -F1 1f I11-1+ -+-+ 1- I- -I- -- I - -I-- -- - I 1 --I .4.1-+ - I-f - -I - --I-- --- 200 00

7

.00000 ++- 1- 1 -- - -I-- -I - - -I - -- H --- f---+4 --- -+I-t--- 1-- - .-!---- - -H-- -I - I .00.00

-10.0. 7 Design Temperature

- -. - l -I I I- I I I F I I I I I t f-I I I - - I I I I I I l- - - -- - I --I I--I I --- 1----i I-I I I I I I I -2I0.00tlData Thermocouple i--f '---- H' - I il 3. CID -U

. 1 ' 000 1000 20 .0 0 02,J. 00 300.00 353 0 -0' 0 ,-. .00

Time (seconds)

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S-' CSS 1ST RUN 48. 0 DEG 51' Filt 1 IIfl .ISOI TIME DrY HR IIII1 SEC MII I.

PLOT HULII-ER 14 T1IM VS TEi'P ZOMNE 10 - FST. PT.16 13 11 10 85 Figure 8.19

A(736T) c(056T) D(Design) E (057T)

.:o0 50.000 100. 00 150. 00 200.00 2 00 300.00 350. 00 400.00 450.00

O l -I- I I-I I II : 1 -I --I i -- I I- I I- I I I I I I 1 +4-1-- 1 11- I -i - -I -I I - 500.00

400.0 2 I-I -I 1 -- I I I 1- 1 1 - lt 1 1 4-41 1+--1 q - I -1-1 I - --- I I -1 -I- + --I ---- I I I 403.00

200. 00 ----I-I -I -- I --- I I-- -1--+ 1 1 -F -- I I +--14 -1--- - I A- --- I-}- 1 -1-I- --- - +-l-- - I-f- - 00.00

D

.hHII----EEI-I {-Ii

. -I-II I --f I f 0 - I F I 1" - I- - - I-I " I I-I-f --- I-- - ---1-I --1-- : - -f - I -+-- -I-I- l-i-I ,1 - 0 00

Control Half-ZoneA Programmer Signal Tenperature

-1o1.-- 1 -, t 1 1 : ,:: C Control Thermocouple --I I-- --- -- 0 00

D Design TemperatureE Data Thermocouple -

C ' 5-000 IrJ 00. 150. 0 2 00 - .00 30.00 3 I 11 I1' I-- .O

Time (seconds)

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S'I CSS I'IT RUN 48.. 0 DEG SISJ I HEitLD Jl I IS1N TIME DlAY IR MlI S.L.C MIL.

PLOT NI.!:::IR 16 1 Il VS 1Eli' ZONE 10 FST. PT.016 13 10 10 85/ Figure 8.20F (Design) c (072T)

. 0 :; 50. 000 188.08 150. 00 200 00 250. 88 300. 00 358.00 400. 00 45. 80

5,00.0i +- I 1-I 4 1 1 F--I 1 1 1 -+-+1-: 1 1 -i -14- 1 J1 - 500.00

4080. C - - I If- I+ I t -----+- I I - +-- I--- ftI 1- - I -+H-+- - --- I I- I Ht- '- I +- 48.880

v •300.00 i-+-- 1- -1 1- - 1- A-- -I- - - - -I- --1 -- I- --- -I, 4 + -++ - I+ ----1-- -- I--I- -I--I- -I-- I--- - +I-- - -1--I { -- 1- -I,- 30. 00

F

F

FF

1028.00 -I-+I----I-f- ---- -- I-Hf-4- -----+ --- I-- - + -I--- - ---- tf- I-I-- -- tf--- -1--A+- -- t ---t --I-- ---- -t-iI--t- --- -- t-I--I- - -- 100.00

S0 -f F --CGGG I

.00r0 -- +-I-t---- -I---I- 1---I - +-f-t----I- -I.- - -- H--- I- I -- - -H--I-+-H --+ -+ t---- -hI- -- H + -I- t+++- -- I 1 -I-+- .00000

Mirror Half-ZoneF Design Temperature

-40.03 ------ i: I I- I I- I-I I I- 1-- -i-I - Data Tnermocouple -I-I-Il-H-I--I--I- -I-H--f-If- - I t t----I-.I I-I-h -4 00.08S Data Thermocouple 0 -

--20 .03 I--I I I IIIIII -1 1 1 i -- I I I - 1 1-- 1 f I I--I- -1-

I 1 I 1 -I-- I I--I I 1 - 1 t I 1 - -200.0o5. 0 5 80 100. ,0 15. Fi' 208.00 2;0.0 300.00 350. 0' 400. io0 . 150

Time (seconds)

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L U:'- C;: IT RLIM 413. DEG S!: lJ HEARID JIEL 1ISON TI I1IK DIY Hf I 11 SI:C MII I

P:01 F MHU..:' R 06 11 [- VS EI1M.' ZONE 11 FST. PT.016 13 10 10 857 Figure 8.212 (737T) 4 (066T) 5 (Design) 6(067T)

i- -, 51 000 100.08 150.00 200.00 250.00 300.00 350. 00 400.0 0 450.00

503 0O I- -I -I I - -I III I-f II I- -I- II --- I- -I Ill 1 --- - - - I 1 f 1 1-- - IH- I I I : 1--I --- I-I. '- I i - 500.00

40 .00 -- -+ -- 1 f-- I - I--H-t-+- I1

-:- I---- 4-+ - ++ -H - - -- +-H-- - ---- --- +-+- I - -- I- -1- I - I- -t

f + I- - 480 00

208-0.00 -+ --+----- -+ ------ +-+- -I--- +? -- t4----- .H--- - f- -- I-4F-I.---- 2. B

55

300.000 -- 4-4-f--- -+- -H--- ---- I-I-- I- -H- -I----l- -F-+--- I -1-I--- +-I--F-H--H----F- I--H-I--- +----- f--I- 300.80

2 0 000 --- +--'-- - t-C---I--I- I- I-- - -- I-I- -F----H- -- --+--I----l--I .+--I-I--- -I-I---I- -I---I-I-f--f-- -I-f-I-$--F-I--- + -eI-I-- f --- I-I- - -I- - 200808

Control Half-Zonez Progranner Signal Temperature

-I00. -11 - 1-l -- -- - -- - -- 4 Control Thermocouple 4- - -I--I---I 1 I- +- -I--I- I -I- H-I-II--I -100.005 Design Temperature6 Data Thermocouple

- 00 I I I I I --

I I II- I - - I I*::e:-I: 5f. 0I leO. 00 s50.00 200.00 250. 00 3100r5 0..00 400. 004 00

Ti.rre (seconds)

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$'I CS'-, i ;T RLIUN -1. 8 DLG Si. IJ 11III. JI I ISM TIE ' [fly HIR N111 SEC MII I.

PLOT HIip':, R 0N8 111. VS 11:-r' 2OIE I I FST. PT. 0116 13 10 18 85i FEgire 8.22

7 (Design) a (062T)

o 100.00 150 0 2-00 10 2 0.00 300.00 358.00 400.00 450.880

500 : ! ! 1 - 1 1 1 H 1 11 4-1 - 1 1- 500.00

4000: I- I 11 I l I- I I I --Ii -FI- -I I i I ---- 1 1 4 - - I I - 400.00

40. 00 -- 1-I I --.-

1:i -l - : I --- I- I H-I I 0

-i --i-I :1 F -. I -i I-.-4--- -I-- -----.- F I I--I--4"- 1 F { H- --- I 1 . 400.00

300 00 4-I- I I i F- --

, I-IA-1-! I-- 1, H-4- Z O. 00

8888 ~---I

05A33 2 -tl-4--I- t-I- lt 1 -ti-i- -I --l-i I-i---i-I I- -I-----I--I -I-I-l t i-I--I- -- I-- -I--t--I---I- -l-----I---I- -I--.-itil-i 2.8880

7

100. _+ i- J +- - i - I- I--I--- I--I- - I--- l--I lI--1 ---- ---v-I -I- - --l - I - - 4-- 100.-00

O.0,3 - 1-- I 1 - - -- - -I -4- I 4 -4- 1 -1 1H - A- - + 1 4 + .00000

Mirror H~alf-Zone

Design Temperature

--100. :-+i 1 : I : 1 it it - - 8 Data Thermocouple 14-1- -t-1-+ 1 - I - -1-00.00

ST:- I -I it I 'I IiiIi- . 1- I I-i-i I I Is-I I i -i Il l -200.00

- 1 0O8 I C f 100190 1S3 i0 20(. 1: 3f::' 00 3000 n 1Ai. ) *t 00

Time (seconds)

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Ut-.U C, t T RUIN-t- 13 D1T h ' A t ll 3l l l 01 nTIMF nY MR 1- 11 SiEC MII I.

I. Il;, R 14 l it: VS .If; ; ONE 12 FST. PI-. s16 13 10 10 857 Figure 8.23

A (738T) c (121T) v(Design) E(122T)

cl: ] 50. 00 100. 00 15 00 20.( l 2:0. 00 300.00 30.. 00 400." 450. 00

5 00 :-1 i 1-1 t 1:1 1-4 11 1 + 1 1 1-1 + 1 1 I- 1-- fI III li-i F i I 1-++-i--' 1 -- H -1 -1 1 1 -i--I 1 i 1 f- 500.00

400 0 - I-I-- I I I -: 1 -I I ---- II I- l--H- II f-I- -1- I- I -+ 1 I-i-4-+ -I. ---+ -FI-+- F- - 1 1 1 - 400. O

300.00 +-t-f-I---I- -I -- F -- +-1 I + I-F -I - , - -- $ -1 - 1- - -+14 - -t --IH--- -I !- - - -4--I -+-t- 1- 0.00

2- .-0 +- - -----FI -I ----- I - -1- -I -- f+---I- i -I--I-tt--+- -- ----- I-I- - -H-- - 200. 0

H--] I I -II 1 I r -I --- i- " I+1-

-00-00- -- ! 4- -- +++1I 1-

( .B00. 00 H - I-I---I : -i t-i ,-I- i -I -- -I- "i-- H -t-- I -, --lt--i - -1- -

- I- H -H -- tI - - . 0

Control Half-Zone

A Programmer Signal Temperature-.- ,e o 4- : r C Control Thermocouple -V -1 A- +4- +-H-1- 1 1 1 I 1- - 0e 00

D Design TemperatureE Data Thermocouple

- 11 - --- i I I 1- iI--- t I -I I FI-i I II I-I III i1--I ll - 20 C00a0 10..80 08 .0 300 350 iiC 4i0:. 11

Time (seconds)

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:F CS :.T RUN '13. 0 DEG S;$IJ HEAlED JEIlTISON T IME DflY HR MIH SEC MILl

PLOT HUrlI:1R 16 TIME VS IEMI .?ZONE 12 FST. PT.016 13 10 10 857 Figure 8.24

r(Design) c(187T)

o .. 50. 000 100.00 150 00 200 00 2O. 00 3007 00 350.00 400. 00 450.00

500. 00 4-I--I-I I I- I I -I l : - .I I- 1- I I -I l - I--I i I---1 I I -I I- I II- I- 500.00

400.00 -I- 4 -F- -- -I --- I- - H- -+- 1- - I-I- - + I- -I---I-q -- 4 400.00

300. 00 -l- 4-I- -- I - - I-I-I- -- - + -----i I-F -t -I 1 -- I--- { -i ---- I--

1

00. 00 F+ +- ---- II- ---- I-I - 2 00 0

IFI F I-Il- i-ffi I F

CG G G A

.00rs0 -- I-- I-I I'- I- --- H---.- - -F-j I- I -I{I ' H,--H- H"

l- 1t

--- I-- -I--I I--I -t--I--- -F-I--- -+ -- I-I--IA -F-H - -l-t-tI---- - -IF----I---I-F---I .e00080

irror Half-ZoneF Design Temperature -- H- I -1000ee

--.. H- +- G. Data Thernocouple

--2 : I--I I -1 1-i I -I I I- i I 0 C T i2 T 1 t- I AII II I200 0. '"00 1 0 3 50 1 i:50 ) 20 i. -:. 00 00.O Oi 4 t :.00

Time (seconds)

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' T C t.T RUN '1.. - DFG - I HER 1 D I1-1 1i so4 TIME lIY HIR NIH SI.C 1111 IPL0OT HlliIL'.:R 06 I llMC- VS IEM i'2-OE 13 - FST. Pl.0l16 13 10 10 85,' Figure 8.25

2 (739T) 4 (126T) s(Design) 6 (127T)

. .' 50.000 1000 50. 00 200.00 2 .. 0 300.00 350. 00 400. 00 450. 00500.0 l - I-- IiI - -I I- -- I -- I - I i-1-1-I

- I :--1 -I-- I I -- I I I 1-- I-I I -l -I I I f-I- I1 I I - I 5-0. 00

400.00 -I- I -I -I -I I - -- - - I --- I - -I - l --- I--I I I I- -H -- I - I -I I I --- -- I 00.00

3 0. N000 -H 1I-II I + -t lF+-- - - 4--- - - -- I F - 1--I-I I 1- 200. 00

1 I00.-00 -f---|- I H -A - - - I----- -- +-- - -- I-I-----

--.- I- - - . + - -- --- - - - 100. 00

Control Half-Zone

2 Programmer Signal Temperature- 00 -I I 1:-4--+- I 4 Control Thermocouple - 1 I-I---l--I-I-- -I -- I-- I- -I-I-I I I f- -160. 0

5 Design Temperature6 Data Thermocouple

-200. ' - - -I I I I I I I I- : I Ii -II-I I I I -( I -- -1 I I - --I-I i1 -I- I -- I- I- I -I I- I I II i !-I I I 2 - 0 .I00

100 000 10 00 150. o - 200. CI +0. Io I00 00 50. 0-F ' H 01

Time (seconds)

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SPI CSs5 ST RUN 4', 0 DEG SKEI HE ED .!ETT IISN TIME DnY HR IIHN SEC MILL

'1.0T lI. IR 08 1II1F VS TEMI-ZONE 13 FST. PT.016 13 10 18 85? Figure 8.26

7(Design) 8 (182T). l0l 0 50. 000 100.08 1.50. 00 200.00 250. 00 300.00 350.00 400.00 450.00

500.00 I-4-I -I--A--- I I I- I-4--I- I --t + -I F- - I- I -1 -I-I-I1 I-- - I--- -I + - 1-1--~-I-- -- I I - -1 I-+ I I 1- 4 5 .00.

400.00 -H I - I -+ --- I-- - -I--I -- --- -- -I- I I - -I-- --- + I I--+ I - I-+-I--I-I I --l - I I+-I 3400.00

30 00 -H -I-F-I-I---I--I I--I---II-I--- I-----t---H -- ----- I- -I----I - h-------- l t----- t--I----I--I-H- --- ------------- - -I-----I-h-I- t- --- F--I-- 0000

,I-(vI--- -- - -I -1- 00000

.000 O ---- F +-l---I--I -+ I- I-I-I-I-- -I--------I- I-f-H -I' --- f - I -f" -1---I -- l-A -A--++ 4-+ - -I- -+ +-- + 1+-+ -I--------1 2. 0

.irror Half-Zone{-300.0: I- I I I ._F+_ I , - - - -- i - .-- -l- i I-l-.- -I- - -i- I -F1 -0.0

8 Data Thermocouple

2-5.13.03i i -I-. - I-- I 1- I I I I - I 1.- I- -1-I f I 5 "-tI- A- I - - 00.00

WOW - 3 0 ±00.00 130 0 300.00 3-4 1- 1 4O.1- -: 08no

8 Data Thermocouple

k j SO 00-0e 00+ 00, 0oOA(0.1A 0 0 2051 f 00 alto. 00 3Y 0040. k' 4 0

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S'.1-' 1 ' T RUN ,18, DEG SK: I.1 HEfltED J-l1 ISON TIME T:TY FIR i111i SEC MiI IFI.hI . -:tR 14 TIIME VS EMIi--ZONE 14 FSV. PI. 016 13 10 18 857 Figure 8.27

A (740T) C (131T) D (Design) E(132T)

50. 0080 100.00 15.00 200. 00 250.00 308 00 350.00 400. 00 450.00

500. -- I I I I ! - I-I I I --1 I - I I - I- IF t j4- 1 I I - I- I ---I I - -I I [ I --- II -I I I I -

500.00

40.0 c -3 -- I- -I - I-- - -1 -I- -H l-- I- I-I- - - I I-- -- -L- + -- I - --I +--I- - -+-I- I- - l l I--- I-- I--I -- 400 00

300 .0% 4-4- + - -+ - - - I -- --- -+-1- tI - 1- -- - -- I-- +- -ft

-l-- F-- -I - -+ - ---- 300. 00

100.00 f-+1--+- - + -l---t f---I -H ---t-I--I------I---I--+ --I~4- - 1-4--H- 4-H F -+ H - --4--- -H-- I- 100.

A A A A

180. - -- - 1-- I- - -1---- I -1 - I- +-I-- f4+- -4- t-- -- l +-+ ----- !--- - - t -l-- --- 1- --+- -+ --- -+ --- -I I-- ----- - 00.000

Control Half-Zone

-v ej ra - --I+ I+ -. 4- -A4I- I -1-1-+.- -.--- A Programmer Signal Temperature F+-+.--I - --- -: - F- -I-I I ----- I I - -1 - 0o. 0C Control ThermocoupleD Design TemperatureE Data Thermocouple

• - .C -II1 I -- 1 - I I 1 ! , --I I , I - I-1 - I -: -I - 0 u

0013 1 01.00. 10.00 200. 00 2.00 300. 00 350 00 4" 00) 4'i0 T

Time (seconds)

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,' CS IST RUN 4:3. 0 DEG S1-.,E I'il- jtI'i SON TI DAE DIY ?R M11 SEC MI.I.

PI.01 .NUI;I":R 16 TIME VS TEMI:'-ZONE 14 FST. PT.016 13 10 18 85? Figure 8.28

F (Design) c (177T)

C. o ;.', 50. 000 100. rO 150 00 200. 00 250.00 300.00 350. 00 400. 00 450. 08

5400.20 1-- - I I 1- II--

I I I -I I I I-I- I I I I- II I I I

+ I I I I--- 11 -

t I - I- I -. I - 5_3 00

4 0 0 .C O - - I I I- - -1- 1 I --1 4 1 -1 - --+ F I I --- -.I I I I . - +I- -- - " I + -1 - I I - , I - ---F- +

vI f - - - -1 - - 4 2 3 . 0

.0 1 + ----- -H-- 1 I -

I I -I--I--I-+ I-+ -- I- -- I - -- I -III III --11------ I4 -1 - -- -- I - -- --- I - +---I-- I I'I--I-

SI0 1 1--i-I -++ I + 1---- - -4 I- + + +

3 00.

00

1 0 I-c -I-- 1 --- +- 1- I1----1-+-- I-I --- -1--I--II I I-I- I- I-'-H--HI---+- -- I-- .

100. -1 + 5tI. Oo 11 ( t - -1-- t-0 0 ,-1 40 --- I -t - --CO - 4 100.00

.030 1-I--- II- I- ------- - -Ti -I-I-- -++- I --I - -+ - -- +-- --- 1--(seconds)--- ---- - H- H -I--I - -+ I - .00

Mirror Half-Zone

-113000 - --I LI--I I-I - I-I-I i F ---- I I- I Design Temperature --- -I-I--I- I I + : :- - c

G Data Thermocouple

2 |i- I1- 1 i - - 1 |_--_:300

0- 5. 00 100 )00 150 00 200. OdE 7 0 . 00 300.00 350 tI -I. 400 Ok -. citne (seconds)

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SF ::-. ' LT RUN 13. 0 DF.G SFI'..l HEALED JETIISON TIME DflY HR MIN SEC MILLPLOT :: .:IR 06 TIl1[ VS ItHIf-ZONE 15 FST. PT.016 13 10 10 857 Figure 8.29

2 (741T) 4 (136T) 5 (Design) 6 (137T)

. . 50 L00 100.00 150. 08 200. t0 250.08 308.08 358.00 400.00 45. 005 .00 L I :- I I 11- I I-i I I i i -I I I - - I --I-: I 1- I- 1- I1l 1-1- -1I-- -- I -- -H F --IH i -1I4 +1 --I 5ea.402

400C. eO00- ++ - 1 1 -IfA I F-HI--- H---- f-- H- 1 -"-+-.FF F-1 1 1 -1- I I I - -H------1- +- I-- 1 + -- + - - 4. 0'

- 300.0 F--I--l---"-I-F - I--I-'I-I -i -- F-I--I -I --I - I--I-- -- -- I-H --I---I300. Cie- 1 +- +4F-I-1- -- H F- -i-1+--+ - 1 + 1- I-4f4-+1+ 4- 300. 03

20 . H *~-FI- I- F - I - l- -l------- f,- -I-I -I -'I -+ +-'-- -I- 1-. -l-l-I F --- - -F- -I-lI--F-I--I 2D010

0. -- -i-H-- -I- I--I F- - --- -- -- ---l-- --f --- F--F-I-II-(- + -- - 1 I H-I- --- i- --- 100 0I

. 0 1H--A-+- !- -H -FFI H-- 1- I-+->1-+ +-t+(-1_-1_" ++ - H-i +-+ 1 1- .0000

Control Half-Zone2 Programmer Signal Temperature

-1o. F I- --1- --- --I-I-l -1, 4 Control Thermocouple [+--1- - - -- 4 I :-- -A -I-- I I I - 0o.ea

5 Design Temperature6 Data Thermocouple

,i T, I , ,i ,1 1 -i i i i T :-I I I I i I -2 (.s cel50!51.0 00 150. CO 20 10 2 , 00 :0l0 [IL 350 S. 00 0 .03

Time (seconds)

Page 45: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

;- C '. T RUH -I,.. O DE G S'l-i, HEI lED JET. IISON TIME IrY HR lMI: SEC Ml I.fLOT NFi; R 18 3 i VS I EM ZONE 15 FST. PT.016 13 11 10 857 Figure 8.30

7 (Design) 8 (172T)

5.; :: 50.008 100.80 150. 0 20. 00 250.00 300.00 350.00 400. 0O 450.00500.++t 1 C-' I- I- d I IA - I - I -- 1- I i ,- 1 -- 1 I -L- I I II-- I I I I -I- I I- I I I +( -+I I I1 1- It 1- 500.00

400.88 -o :I---t --- +-i- - --1- -- I- - -+ +- --I- Fl -1 - - +I ++- i -- -- ---- I -- - -I- -4--- ----- 1- I-H-- - -- FI- -H- - -1- --- - -- -+--- I- 1i--i f- 400.00L

3066 .00 f+-+-4-- - I 1- - --- -- l ... - '- f- I --- .-- - .- - + - -+ ----- +-+-+--- A4 ~- i-- + -1--- -1 - I+-1-H - +q---1- -I4-H--+-.+-4-

300.08

o8 Data Thermocouple

a I2W 0 . _I_+ 1 I-4-- I-! -- I i --II- - 1 I -tI------I-t-( -- ---- I -- 4-1-- -- I-li-l - -+ --I- -i+4 - 1 1 -- 1- 1- f -200. 0

S.10. -0 I.--.00 15..0 21.-I0 250.00 3041-+- 35-.10 4-0 4 . 00 0

rrr Halfcond-Zons)

-100.2 --- I i -: t :: I- F I I i De-1 I I I ? Dsign Temperature I-I-- i- -t--- t I--i-- ---- iI I- 1-i-- +1-I--I 1 -1-- -100.008 Data Thermocouple

!-I I i i I I --. J i I I - 1 -f t i IiI r i i i H I i-: i-ii-i-i-i I I--221. 00L100 any 'I.P. (10 15. Pr 280.1 )0 250. 00 350.60 cBi 0 4-A. 00

Time (scooncs)

Page 46: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

-,T .:;; IT RUN 48, 0 DFG SKIFll HEllI ED 1S0, TI ME 1IY HR 111I SEC 1111.l_S .R 14 IE E 16 FST. PI.016 13 10 10 85? Figure 8.31

A(742T) c(141T) D (Design) E(142T)

,- 50. ±0 .00 150.00 200.00 250.00 3008.00 3501.0 400.00 450.00

S0 -F-I--I-I- -- - - I-I---+ -I I--I--- +4- l - -1t--H-I-+---1 I- -+ -H I--+- -I-- --- 4- - +- I---I I- 1 -4- - I - 40.

g4 300.80

100.00 -I- I-4- - -44 --I--4---- -- 4 --i--- 4 -I-- 4-1 -I---I---

--- -- I-- - - - +-o-1- -I-I- '-I -+--+--4-1--- 0.00

-I--f--I l If -

II- -

t±-f-I---F - f--$- f.- - ---- I -- +-+-I---4- -f--F- -I -I- - -

.0000 a 4-I-II-I " I--I-I -I - I-I----- I -- - - +- - +- -I--I-- +-- --- -H -f-+ - - ---- l- - --l .000

Control Half-ZoneA Programmer Signal Temperature + -I-I++-- +++ - -- oo. 00

-a.e -:- - - C Control ThermocoupleD Design TemperatureE Data Thermocouple

-4 :1 1: ~ 1 I 1I- I I I I-I" I I I I II II I II I I I I I I- --200.00

- :03. ., I-1 I 1 1 0. 0 I 21 3. 1-I I I . I -0 . I-4--. - 200.

. : 5 000 1080. 00 150 00 200. i3 250.00 308.00 350.00 400.0 .;,0.00

Time (seconds)

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Pf CS. I-ST RULN di, 0 DEG SII'L HEA1-D .IE'TISON TIME DIY HR MIN SEC MILL

PLOT NUI't'R 16 IIME VS 1EMP-ZONE 16 FST. PT.016 13 10 10 857 Figure 8.32

F (Design) C (167T)

1 5 000 10 0. Co 150.00 20. 00 250.00 300.00 350.00 400.00 450.00

500. 1 - I : 1-I l 1 1 -- 1 1 1 1 1-i- I I I I -- I I I - I -- I 4- II-I-I I -1 -i --I-f - - - I I I- I-+-1-- 1 I-- -++ ft I--- --- 1]-- I >-t---: -l-l-I- 1- 500.00

400.00 r - - I-- I -I - I ---- I- l-I--t-+ I I--I- + l----t I -f- 4I-+1t H-Hi-- - I- -~ -H - -I+-I .I-H-- - I-f --.--- t-I-+ + - -I-i---I--- 1-! +-tt -I--I- I I---I. 400.00

- rrvu.I} Ttfi IfF ~TillIbIIlif-lG G G G EFFfTlIlW

E- 20 .00 -I-1 -1-1--1--i- I --- -- I--.FF F--- - -- ---- I---i-A - - -- I-- 1- 4- t-I- - I- -I---I--- --- I- 1- 208.00

-00. --- I-I-----I--'l--I -I -I--I-'I--I- t---I-I-- -I-I--I-I--I-I-f -- -- I-- I -- H-+----I--- -- I--I-H 0 .00

100. 00 ---F-i-I- - + 1 -1 F-f1--- ++I-- +- +--l - -+-1- + 1- 00i

0 I00 I--- I - I--I -- t- -I- -- ---- I- -- - - - I-- '-I- -- I- I --t -- -- -- - A---I---F+ -- -- +-+++ + +--+ - 1----I+- +++-- tj . 00000

Mirror Half-Zone

-Ii. 0 I-1--1 : I I I-I i I- I- I I g -I--I -I -t- ---- -:--I--I-- --- I- -I--o-I - I- I II 1 --11- -100. 00

I -- |l i-1| I ? 1 1 : :-1. 1 I- It G. ' i-1 iI 1i I I 1 .1-- 1 II I I II - 1-1-1 1 I i-tf t i-I -I I I I I 1--200.00

BOB. ,: 00S . o .1 2s1.1 '0. 00 300. I0 350. 100 40fi. (0 4""1.

0

Timne (seconds)

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'F CSS IT RUN 48,. DEG SI K ~lI I Ilt1) TlV1I SON TIlE DOtY IR Mill SEC IILL

PLI.1T 1Hl!i1 R 06 TII1E VS IEM-' -ZONE 17 FST. P.01 13 10 10 857 Figure 8.33

2 (743T) 4 (146T) 5 (Design) 6 (147T)

.: 50. 000 100.00 150. 00 200. 00 250 00 300.00 350.00 400. 00 450. 00

5003 1-I--I I I - - I i --I I : -II -- I I : II-{ I I I 1I - -I - l I-I--. -I I-I I VI I-I I- 500. 10

400. I - I - II-I I IH-- -I I -I- F II 1 ii-- I -- H- I -H-+ -I I-I--I-I-I - I I-I -I 400.0

300.0 H- --- I- ++ -I - -1- -H-f- I -+ I - i I--H H- F I-+ H-1-F1 I- i-++++ -1 300.00

20. 000 H--1-Fl-I- I -I --f- -- ! f- -+I- I- I I-I I 1-- -a Hf I A- f F4_f + -- !-- --t -1- -- -- 200.00

ltHi3I __ . ± l otaOO

13. Ca j 0 I-I ' I -I,-I - ..-- - I-4- I--'--I -I -I--- I---I I-{ I- - -- II--- H--I- I-I : - - ,--I--l---I - I H-- I - -F-f-i--I -I-l----l -I- I--I----I- , --

0 II--I-t I- i A 1-1-+- 1 + -1H i H --1i I I- I i- .00000

Control Half-Zone2 Programmer Signal Temperature

-l00d I I I -+ 1- 1--1 4 Control Thermocouple -F F -1 1 - - -100 -o

5 Design Temperature6 Data Thermocouple

II i -i i t , I !i i i I - ! | - i i i -II i i nn0 -- ' 100IC.00 15A. f0 2k. fir . 00 300 00 350 00

Time (seconds)

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-,'i CS '.T RU N 130. 0 DEG SI: hi HEI-I ElD JI:TI IfD TIliE DI)'Y fIR l1111 SEC MIrI.

O H ; R IS 11I.' VS 1EMg' ZONE 17 FST. PT.l16 13 10 10 85? Figure 8.34

7(Design) s(162T)

50. 010 100.00 150.00 200. 0 250.0088 3008.00 350.00 400.00 4510.00

500.00 1-F- 1 1I I I- --- -1-- t -1 1 - I A I-i I -I --f+ -I I {1- + -l-- -H-+I - - - 1H: I -+ -f --I 580. 00

400.00 - - --- I- ---- + 1 ++--- -I H-+- 1 i- - t-+ -4- I--+ --- + 1 +-I -- 1-+-I - 1-4 -I--- 488.00

300 00 H-f-I I - - -i- -++-H . - -1-- -- -+ -- +- I -+ - -H-H--H - i- -+- -f- I -+ H 4-+- 360. 06

100 00 H-H-1--+- - 1 -4-+ H-H - -I I"---I-++ F --+ + -- FI--I--- + -1 11 1J- - -H-I - - - - - 26.6

100030 +I-4- -I -- I -I t 1 -I- +- -++I- - -I---F + - -- - -H-+--- 4F--F .I -I- - -H- - I-- -H---F -4-1 - * 09.0 9

Mirror Half-Zone

- -0.0 I - I-f-- -I ---- I-- I I -I---- t- -I 7 Design Temperature I- -- u-r - -+ - -l -I --H---I--I-I. -0.0

8 Data Thermocouple

-20o00. -2 - I- 1 11i-- I -I I I 1--I +- ----. --- I - I I ! I I I I f I-I - -1I 1--1-I- f -- i 1-I-I--I I . .-I -- I- - l -- I-I I I I 1 t - -200.00

..:50. Bee 100. O0 1 . 03 2 0. 00 258. 00 300. 0 350. 00 400. 00 450. 00

Time (seconds)

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F51-:' CSS ST RUN 48, 0 DEG SKEIJ HEnILED JETIISON TIME DAY HR MIll SEC MILLPLOT HUlt. .R 14 TIME VS TEMP-ZONE 18 FST. PT.016 13 10 10 857 Figure 8.35

A (744T) c (151T) D (Design) E (12T)

.0.:'03 50. 000 100.00 150. 008 00.00 250.00 380.00 358. 00 40.00 45R.00500.00 -I--- I -I ---- I-.l -- I --- I-- : -I -I I-- I I-I- -- l--. I I ------ l- -- l- I- I -l---l- I -- I ---H --.- -I-.--- -I-+-4-I-- I l--I- l-- I- I- - 1- 1r------I I I - 5 0088.8

400.00 -- H- I- -I--1- I--- - --- '- -- I--I----- I I 1+- -I -I-- - ---F- --1t -I--- --- +-- -1-- f-- ------ 1--I t- 400. 00

300. so "- I 1t- - '- 3200. 00.

i 3. -I--+- - I- --I ---- l- 1 +- t - -- - - I- - - -- I-I- - t .- l- , -- - tF-+ - -- I-- I-- '- 21 0

Control Half-ZoneA Programmer Signal Temperature0. l- I- I-I- FFI--I - -+ -- 1-I C Control Thermocouple -I- - -I---I I- -l--I-.- -I-I ID Design TemperatureE Data Thermocouple

:50 • 000 1 .0. O 3 150 00 2F10. 0 2:7 . 00 300.6 ._ 1 E r -1 .

Time (seconds)

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'1 US'; I T RUN 41.3, 0 DEG SKI. I HEIIED JLTTISON TIME DNY HR 11111 SEC MI.LPL 01 Hi.:;:I R 16 1 li11 VS TEHI" ZONE 18 FST. PT.016 13 10 18 857 Figure 8.36

F(Design) c(157T)

., i'o 58. 000 i0.8 00 150. 02 200. 08 258.00 380.88 3580. 0 408. 80 450.00

500 I + 1-- - I-I I -I - -I I I - fI - I -I F 1 1+I-I- ' -- I- - f- I--I--f4-- - I.- I--F- IFf-I -I-_- -- I II I1- 503 08

400. 03 --+-)-- -lI- I+- -I ---- + --1-- -f-I -: -I--+ --- -H- -F- + i ++I-++ -- + -+-- - f--I 4--H-- -4++---+-F+' l--F+i-H--4----l--Il-+- 400 0

300. 00 - -++ ----- +--I- +4-4-+- -F -- ---- I---- - - f-H--_-l---l-+ -I-I- -+ - If--+--f--- -+- - I- 3 .

200.00 -- I- - - I- I -I-f--H---1- I--I- -I - - - --- +l--i- - -F+I--f--I--- - --++ + +-I-I -- 20.00

600. -- + -4-+- +- -+i----+

--- + -f+- F-+ -+-I -f--+ -- +-f-+- -- H---+-' H-1 + - H -- - -- t---I- 100.00

.80800 -H--I---I - -it--- I-- H-I- - - - -- f-f-- -H -A-- -- f--I- +- --I- -- - 1- - ++-+- I--,4----+- --- +- + -- --- - ---f----+ .00000

Mirror Half-Zoneij F Design Temperature --A

-100. 8 1 I-3-- I- -I -- I-I--1 - - F Design Temperature -- ------ I I-+-- -l--- I-f-----F---II-- +--F-I--I---I --+l100 O0G Data Thermocouple

-200. 01 1-lI il- !-. 111 ! - l I l I-I:-AI+-1II 111 I-ll I - + i I-- 1 A III I14 t-1- . IT Il - I fI i I f- -230 CO. IO 50 800 100. 00 150. 0 200. 00 200. 00 300.00 3500 400 00 45u. 00

Time (seconds)

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Figure 9.

Power history for heating zone no. 1 power controller.

t

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Si'F ESS I;T RUN VS. 0 DEG S5.C I[ L it TISON TIME D:Y HR FMIN SEC MNI..PLOT NU :': R 01 111 VS FPO O: : ZlUN 1 (I S.M.7:6) FSf. PI.IIG6 13 10 10 857 Figure 9

i

5.M 1 5 000 30I 00 . 350. 00 40".( 4r'. 000.r i-i- l: I-- F l I--I.l I - I : I - 1I : .- -- I I : - 1 j-- ; . - - I- - -I : $r.0p7 1 _ * .

.i -I -I I--H--- -l i I- .- -I--- I--I

.-- I-I- 4 0.800

S 0- -0 I- i-I l---I- F

-I--- -- - I 1 - 2II 0 0

-InO .0- I -+ 4 { --1 - I - I- -I --- 00 00

:4 0 i t 2 I--I-I-I -Fl-i-- $ - -3 .n 3 0Sti

0 i0.0 -f--I--- - +i --I M --. { -i --- j If- -- -i-f H- i-I I ±og. 00

r+ N +f.

r ON. K vI - : i :- (Ii tF! 1 J 4-' 1"1 1- 1-1 1 1- 00-I CA --- I --. !-I I -:-I- I I I I I I I - IT 1

G. 3 10, 1 . 130 2. 20k f; .o 0 20. o0 3 ,rl , V0 - 0

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Figures 10.1 thru 10.40.

Design and data thermocouples circumferentialtemperature distributions.

I

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L:'I L:' I'.T RUN 3. El UhL '1' ', III f1 1 11 U 11 11 ' 1IV N TIMIE l f':Y li: MiH SEC Hi1IF,01 it I-.' R 0:'? f. iI VS 111E i T;' 2' . .TI 1E 10 FST. P .U16 13 1 10 St,, Figure 10.1

i (Design) 2 (Data)

. 50. 0010 100. 00 150.00 200 0 2'..00 300.0 0 .350 00 400n0 4: 005C10.) 03 -II I I I I : I- I II I I I I I-HI--- : I t-Il- I I I-- -F - I: l - I1-E f F I- 1 I - I I --+ li -t-I- -- It - I - ,00 0

400.09 -- 1 -I- --I I I H I F-I --- - -- I 1-- -I I-f -I I-- - +4 -- -I-I - 1--I-I-I -+ - -I---II----+- I- I++- -- I- 1 I-F-+ - I- -- - F I -I - 400. 88

400.8faIt - 1 HH ! -1---1 1-- 1t 1I- -I+- - - - - -F---I-I-I - 4200.00

- .0.000 - I-I I 1- 1 1 1-I-I-I -I - t -I--- - I ------ 1---- I - F- 1II-I-- - -I - 1-- ---i - - +(- - --- IF-I- - - t -I-- F-t- I-+-- - -I- ,

I - 20000

1. 010.A0 1 -I- I : I 1 I1- + F -lA-I1,

I I -+-14--, - I I 1--H- f- --- -I - -I- I I----I--I- I I -- - 1- l-- l I---I--)-I-F --- -t I I-H -- -I- -- --- -- -I- +-t-I--,-- '- I--I .0+

oo 0u. ::'-O I- I I I -- I I 1 I----I-I-I -- I-t f-I I I-I '-I I I- 1 1 I-I----I- 1 -- I- - -I--I -- I -- II I I - I 0000

4: I t Ht hI fII II I-Ilf 2 I 1 +1

F I- I -I 1 - II1- I-F1 H IIA iI. II00Q J.50 rli 20l. I-- 300. C 4 0 t W0 i. t h

Azimuth

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I- :.,;: T RUN <-S. D[-.G SKI l !HE L F- I .1 II 1- TIME 11 FP Y r 11 i S[:C M11.,.OT NI-_":ih R 82 All VS 1 l".' STIn 22F.1,TIME 151 FSI. P '.116 13 11 10 857 Figure 10.2

i (Design) 2 (Data)

. C.: :. ,0 00 100. 10o 1508. 2008.00 250. 00 300.80 30.08 40. 00 45.. 00-0. i-' I : I I I- FI - II --1 1 1 - 1 I I I 1- 1- 1 1 --11 1 -t III I - 50 0..0

420.00 "I-1-1-f I I I - I ---1---F I I1- -1-1 -1 - 1 1 FI f -I + I 4 -t- 1-1F-I 1-1 -H - 1 1 1- -i -I 1- 400.00

+ I2 -. 1 --I-1- 1 F I -F - I-I 1- - -I- I I -1-- 1 - 1F-II- I I -I--i- I -I---1 F---I---I-+ - 1- ----- --F--I-

- -- 1 - - I---- - I- -----I --- I - 00.0

1. 0, -II III I 1- I1 - I -I - 1 I - I ---- -- - I- -- + - + - -+---- - --- . -I - .00.-000'3 -- t F- II- I I -:F- FH-I- .- I -I-- -I- -I-F --- F-I I---F- F-I-F -I-f.-1- I -H I--I-I 1-- - - -f-I--I l-H -I-l-- l-t-I - t-- --- - -- -- +--F I--F- --I -lf- -I-I 1 - I I- --00.000

-1I -- ll I .1 - tI F - -I F I- I I -I-I- -I F I F- -F --I-F- I F F I- F I -- 1 -- l- I-- --tFl --I I I -- l I I -I -200.00

5 01o8 I0. O 1is. l0 200. 00 2513.00 300I. 60 35C 0i ".' 4' "tAO

Azimuth

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'tap (zS. .rT pLIM .!-. 1 DE G So. I HI t D A: 1 lbIll TIIil P Y ip HI l I .SFC 1111 IFfl HiM' R 02 WIl VS IL' S A 2- .J I.TIME 'I FST. fPI .16 13 10 10 8,s Figure 10.3

1 (Design) 2 (Data)

:!-I 000 1 n00 is i 2- ' 100 300. 00 3 h 'l, . 4 .. 0{i IJ {~- ! 1< I:- 1 my W20

4C0. :-1 P 1 F-1 H il 1 400 00

300. I I I I - I -I I I I I I I - 1 1 - 300.0_. I I I -1 H : I .- :- P t-+ --1 - -1- too. 00

2_2I2--

I't- I- i 1 1 I :-I - I ;- N-... I. t 0{ 1 i I t - -I I v- i I : I l-O- -I --I- { I-----I- I -1- 1000

-00.- -l- -l I I- 1 1 I I- I. I- 1- I I 1 1 -A I - 1 + 1 1- 1{ -1 I I 1 F- 08 00

.00.." t: - I I I-HI I I- I : I -I- -1- I-I I I I- -I -- I I I - i t t i - I --t- -I I i.- - - - H - I--I I - I- - t1- 1 :f-I. .I: 0o

l- ' N 1 I 'I I N I -I I-I -l- -- I "- --I -I I -I |- I -II'I -I -0 1 1- 1 0 1

..

. .- "- , -I J 1 1 1 1 I I 1 1 11 . I"I I - I I5;i t li. 00 150 t0 21- 51 2-". 00 300.00 3S 0 t '. 13 '1 .00

Azimr:uth

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'bI C . I LT RLIH 18. 0 DLG 51 I. HEl- J .1 IIIS ON TIHE llY HiR 111 SFC 11111.

Pt IU i ;.: R 02 A. TH VS L t T;' . 2- . .TIME 241 FST. P .0 16 13 li 10 85e Figure 10.4

1(Design) 2 (Data)

.r50 8013; 100. 08 150. 00 200.00 25 00 300. 00 350. c400.10 4iO51. n

50A.Oi L - ; I - I I I--- : I--I I I I I 1 i I- -I II I: -l I I--I : ' - I: I - 500.00

4+.08 - I-I - II I I I I-I- -- I +H'. I - - - F IH- -+ - i I l -- I- + + I 1- 400.800

00. 00 -

-- - - + - - --. -I--+ --------- -- -+- -F-1 H tI--- 1- 300.00

300. -- H 4 1- l -1--:-- - - + -2 .4-t

2

108.00 HI - --i " "- + -0 I-+ -1--4-- 11 F i --- - - i-+ - +H-- --I+ +-1- 4-+ -i- + + 1- 00.00

0000 I--- iI -I I I-I - HI- -- I - -I --- -1 -1 - -- I- - +- -- I--1- --- -I-H- I - i I- -I- ---- I-I I - .0000

-10 -1 -I - I- I- I - I-f +1+I 1-- I -1 II ---1 1--I---- 1 A I-H--I t-iI1- - 00.00

- I - I - *-: :- I| : 1 I20 I--.I-i I I I-I-I '1 1-10 1IH - -20005" 0'i) 10-. r0I 15 10 2 00 2". 00 3<00.00 350. -100. _-I 00

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F L-, RUN IS. 0 DEI. 1.1 I R lAll D II ISUN TI 1 I 1, :YH' ' il lIN SEC 11II L1 ; .,: R 0 2 fIM VS I TP ' ... TIMV 2b F;1. F'PI.1 6 13 10 18 85i' Figure 10.

1 (Design) 2 (Data)

II L 3U U . O 0 I . 2 l !1 ,' 2 .2 0 0 3 .iu t :- ' " , 5 0 I, l t ( 4 . , 0 3

VI 0.-I I oI 0 1- i - I i1 : o . 1o f

300 C11. ..

- I I I: - I - ' I I- -I i -I I ISI i I i i- I i

1111 11 j Pi

S[.. .1', -t t +' - I -I I I 2 0 0 .0 0

2

2

. I 4 I- I I- I--I- I- --I I I -± .0000

80:0 -i I 1 :-l -(1 .1 I-n :- iI I-: ( I 1-- I1 noo.0

.s. . .I ' I n2 1 :7I l , 0, ,3 i 0 0 3,t, 0. . '1 . 110. . . . . . ... . . . . . . . . . . . . . . . . . . . . . . I- I I I I I I I - . . , I . . . - ,- b -:'

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' C T RUN 48. 0 DEG SKI:I HERIED .IIISON TIE MY HR MIII SFC MII.L

HOrT ;;R 04 AIM VS TErP STA 2511I..TIME 100 FST. PT.016 13 10 18 857 Figure 10.6

3 (Design) 4 (Data)

50.001 100.00 15A.CID200.CI 2Zif. 00 Z00. 00 a50.0I 400.100 450. 00

S30 i-i-I i I - I I I -I- I +-- I --1 1- 1 1 --1 I I I -1 I I II- I I I -- I I- I 1- 500.00

400. 00 1-1 I1 - -If- I --I --I 1-V-- --I--lI I- I -i --I i -- 1-- -I- I H--I-- -- 1 -I---I I- 400.00

D - I- I-- F 4- - - 4 - i+- 1 200. 00

200 .8 ..... .... 4 --- +-+-I-0

4

i0o. 00 -4--1 -1 - 1--- -- f--- -----

- 1-1-f-- 4+. - + - -- +-

tc. 0 -I - II-t- I- ' I I- I 1- --- l-t -!- -I-l- I-.- 1---I-I-I H - I -I--I-I-I -- -I- -t-t"

I---1--"H -I----I--- -F- +-I -I-f t H--l - ---- I---- I-Il-- I-I - .00000

I II -1 --1 1 1-I+ 1 1 14 1 - I 1-4-1 F1 I1 V -I--- - 1- 1 1 1- -O 0.0

I'i O 3 100 C 150. fll00. (10, .. 3 0r0 3 0 l CI -0 .

Azinmuth

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'PF LS ,;T RUN 40, 0 DEG SI'l.l HEATED JEIm1rIS TIME DAY HR MIINI SEC MII LFl 01 N.tj; 1

!FR 04 AzIM VS IEM--STA 225 i..TIME 150 FST. PT.riI6 13 10 10 857 Figure 10.73 (Design) 4 (Data)

i s 000 100 .0 150M 20u. 0250. 0 300.00 350. 00 400. C0 4'.. 0050 -

I0

[.0 J H 1 I - I : II I I- I I - - - - -- - -- I + III -1 - I H I 1- 500. 0 3

400.0 - -I -I I I- 1 1 - I -1 -I iI-I " -+- I I _F- 1 1- 1 --- f- - --4- 1 1- 1 1 - 400.008

300. , F - 1- 1 ' - -- + - 300.

CD +

-+ .- 1 F I +

- F--I 1- I - F t - -I -- 1-I - I - -I- I F -t

- I- -- I "I +-f 4--' -- + 0 . 0

1C.C 00 -- Ii 1 II +- -: -+I- I 1 - 1 4 -H-- -- I -+ - -4-- - --I -i -I -.--- --I------ 200.00

i -

. C + 00000 -H I Il { - - --I - t I I 1-t- -I I - -11 " 1 +-I 1 ---- 1 1- 1 -1 + I I t -0000

!i i i- i i : i- HI T t 1 1 I I~ II- -2110 i 00.,00, 100 .0 1 . 0 200.: 1 0 300.00 30 .l. I' I - .1

I- (- ' I I 1-'-- I G- '1 " 8 +1 6 I ) - I- 2] -l 1 -: I-I-"-. 1 - I +0+ I I I--) +I .

. '+ 1 -- 1l "; I ~. 0

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:: CS. I,T RUN 118, 0 DEG S .1 A [I IEl I 11t If ISC TIME DW HR Mn114 SEC MILL

PLOT Ni, R 04 illl VS 1Mi STFA 22Sn.L.TIIME 200 FST. P1.016 13 10 10 857 Figure 10.8

- (Design) 4 (Data)

S5. 00 10000 0 150. ro 20 1. 00 250. i08 300. 00 350. 08 400. 00 450. 0

500. 1- IiI I- II Ill-i t-' i -- 1 I I I f-- I- -I-I-- I-I ++-+ - I 1 -1 -I -- I - 5O. 00II4 3 - - --- I -I I-I - -- -1 - - -- --- -- A- A-+ - -H -I- -I-- 1- 400.80

4 - 4

4

-~54-

S 2 f0. A 4--I- I- ---- -I-----I--- -H-4---- + -+ 1 - +--- FI 200. 00

-00 .0 -.---- 1+- I- I- --- I -I----I-- -I- -I -- -I- -- 4- --- f F-I- - -I-I-4-I--I-I-I--- --I--- -1 H - I-I- H -i-fF - l--I+ I 1 - 100.00

0 Qr-- -I-- -- I--+- ----I-- 1-- -- --- 1- I ---1 + -- 1-+- -i - -I A--I-I--I4 I--- - I--+-I-I -- -1- - + - I I --- - .0000

-00. 88 l--l-+-I -II I --III-I- -I- -I- Il - I- I--I I I l-----l- -I 0I--l0-l--8-I

-, l- l- Il I I f- I I -f1 -11--1 1 + 1 -+ 1 I i I i-100 i " :-I 1 1 1 1 1 1 1 1 1 I --- I 1 I- tI 1II 1 1 " 41 -- I -I1' I I I Ii 4 -1- -i1. Oe

5 OR@ io 00 150. 00 2 250. 0 300. 00 350. 00 CI1 0i.

Page 63: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

' C'.-. :'T RUIN I., 0 DEG SK LhL IH It:l) JI. l ISON TIME DRY HR MIM SEC MIIL.KF IH -:.; R 04 nA. IN VS TEMI STA 22,l .n:TI1ME 250 FST. pfr. 116 13 10 10 857 Figure 10.9

3(Design) 4 (Data)

C.. 50.S 000 100.00 150 00 2.0 20. 0 300.00 3500 4A. t 40 ,0 005 L0. I I I: 1- I I -I I I I -- ,- - -I i l-II! 1-i -I- I.i F t II '-- I I - 5(0 00

4v. 0 3i: I I- 1) i- 1 ---1- -1 I - -- i I-I -- I -4 I -+- ----- H--- 40.0

z111. 3 - -F F--i--I- 1 1 ,-- 300

20 00 1-1-1 t- I I I I-- 1 I-H-- 1 F- --- I 1 -I -- - - )- - -- -- 20000

100 .3 I - I - I--I--I II I - -1-1 ---- I-I-I - 1 I-- -i -I- - -- F -f- I -- I- -- t--I-- -I - - 1I 100.00

S- -1 -1 1 1 000

-10 I I I- 1-I -1 1 1 1 I i4+1--1 4I-

A I I 1 1 -4-I- 4--I--- f 1 I -

I- I- - 1 I - - 0 21-0

Sf 00 300i 3 03

Page 64: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

.I.'F R.;: ; 'T RLQII ':13. .l DEG SI HEA II i) If T-IS1ON T IIE L I)Y ItIR NIM SEC 1i II

OT .. R 4 . . II VS IEM STA ? . .TIME 2?i FT. PI.016 13 10 10 857 Figure 10.10

a (Design) 4 (Data)

o 5 100e .00 -201.00 250.03 3o00.08 350.00 400. 00 450. 08

5006 O , I . , I -- -I I- I I ----I "t -, I - - - I - - 4 -+ ( - - - - I I - I ! I- 500 , 00

-)-- I ---f- -i H I f---I-'I-I---f I - -- I-l- -- I- + -I---I- - -I--- --- - I-' -l-I'I- I-- - oM.804400-- -II 1- - I- -- I - I tf H--a l t-- +00

4"

30800 ---- I - H-I ---- ---- -I-I---4-----I I- ++ -- - I- - -- - 8100.00

4 2 !800 -I---+-I,-I--I-I I l-I--I--I--- .I- - -I I---I-I-I- I- H -I-I--I I--f -+--I-i.-I--f---- -I--- I-I-I----I- I--I---I-I---I-I-I -. I--I--P -, I -I--I-A 2888

2000 -I - +-I- I i -+ + -l i -H - +- -----I0.-+++ -H--F+ F- 1008

-400.-0 - 1 II I F I I + I I - I I I- I I --- I-4- I -- -- +-HII 1 I--- -- - I-- I ! - -I F 1i Il 1+ - 0000

-4 ur 0 1I I:- I I II- I I I-- I-I I I-I I I--I III -I I I II l I I I - -200.00

. :'1 15 .r L5 '2 010 250. 0. 3 00. 350.00 . 0 'I' .0

Page 65: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

F , -:T RUff 41. 0 DUG II -iU H I IL0 I I IIISO.N TIME D:fY HR MIN SEC MILLI'l F 1 .:R 06 f;li VS t .10 A .-- .0.TI'E 11,,-i FST. PT.016 13 10 1 857 Figure 85CO.

S(Design) t (Data)51j. 000 10 00 158. 00 20008. 2t3. 00 300.00 358.00 4800. 00 450. 0

400 "- I - 1--F-I- I --- -t - i - I I -1-" - -I -- -I-- - I - I "---1

-III -I--+ II +I-+--I-------- -- 4---- I--+Ill- --0. -0

Il -I-I-I 1-i I- 5 400 00

0. -300. C3 - 4-++ - 1- 4 I W-I---- --I-I-I -+---- ---- I - "I---H ----- II- - +--I--------+ fI--I--i-- -I --I - I--H--+I -I-I--I-F--F-I--F ----- I I0 20 00

t

200. 0 H--I I--- I -

- I--4- i ---- -I I -I----f-I-i--I-I--I- ----- I--I--I- - ----- -I -I--I-i-I--H -- 260.008

.00.00 -+ H - -1 -!- - + 4 ++ H 1+++ +++ + 4-H-1 - + H ++- He++: H+- t++l+ I I+f+ -----1- 1.00. 00

0. + -1 1 -- I 1 1- -0+++- - - -+++ + -4- 4 I ++ 1 -- F--4--+-+ 4 -- -1---++ + 4 - 1-++4 4 A H 00I00

10'0.3 ---- I I--I- I-I-, -I--F-I--I-i-I-F- I F -I - IF -I-.-I --- - -I-HI-f---I-F -.-I- --I-I---I-I-- I-I-- - --I- F----I-F-+-- -I-- -I-- +-I---

-I-- -F-I---H I-I-- , I-I--- I- -- 100.00

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-' i -| I III Il -I I I I I- I I -I- I I I l I-l I-I I I -I- t-- I -I I -t-- I I 1-l--|- 1 44I-I-I-I I i 1 I- I I I l - -203. 00

j.0 1 .00 1SO.) 200.0 250.30 300.0 350.00 00A 45. 0thA7.iiruth

Page 66: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

TF CtS I.T RUN 4, DG S -6L HEllED JETI SOM TIME )fY I.IR MIH SEC tllI LFI.-T f:;:i.' R 06 lIl VS IErli' STA 23b5.0,1TIlE 150 FST. PI.016 13 1FI 10 5 Figure 1012

5 (Design) 6(Data)

'. .. I 5. 800 1 00 150. O 200. 10 250.00 300.00 350.00 400.00 458.00

5610 3 -+1 I - -I I-- - -I- - - l 1--I-I-I I - I --- tH I- - - - I - -I-I -I- I - 500. 00

200.00 - I- -- I A -I-I- ---I --- -- It-t- I----m- --t-I

- l-- ---- ---+-----+--i- -4--11 200.00

140.00 I1+ e- l I 4 -+ 1 - i t - -t-H -++--l+ I-I --- I---+A -I f -- 400.08

.-0'B -- FF I -I 1I--I .-- - I II--I---- I- - H---t-----t t -- 1-- I-- I- - -- I--I -I- I-- t--I- - t-- I+- --i - - I-- t I - 00

-A- - -HF I .80000

1 10000 -I- -- I- I-I I I--I -I--- -- I I- I-I1 -- I l--I-Il--I-- IA -I- --- - - . - --- -- --+-[ 1--+-I- - ----- -- I-H - I I .- 00.00

-1.0. ( I-I--I I I I I-I -4--I .I-I : I I--f- 1 I I-I--I-if t I - l--I - -I- --- I-I-I I I--I--I--I- I--H--I-- IF I- - -I .I I-I -100.00

--. -I I 1 I I I -I I II I I I I I l- : I I-I I I I I I-I I : : I I I-I- I-I I I I I I--I-I , I I I I-I-.-.--I 1 I I--II- I

I II I-TI I I I i i i 1--:M I 1 - I - 1.100. o" ' : . 10 r .. rV - o 201 *. 1 216. 00 300. 00 3: . 00 -IL). (1I -I .00

Azimuth

Page 67: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

'Ff '. .T RiN 4 .. 0 D G S [GI H[ HIlD JIFl IlSUN TIME I;Y H-R illm c- MilPLOr il:, i R 6 IiN VS 1L0f' STA 2.Ab .[".TIM'IE 2'1I FSTr. P lt1 6 13 I1l 10 85' Figure 10o13

s(Design) 6(Data)

,) 000 100.00 150.00 200. 00 210. 00 300.00 350, 00 400. O0 451:. 00

4001 00 - 1--I - 1 -- I I - I -- -I II ---- I- I -- I- I- I --I --I I f---I -+- I- ---I- I I-I- 400 00

M0CI.00 -II - - - - - + ----- -I -I -- I-- -- l- I---{- -t- -1- ;-- tl- I-- -I - 400

0

100.00 1--I-- -f I-I - I- I- - -I -I-- -- -I 1 -- f-f - -- 1-- -I-- -tI- 1-- 00

00000 - F1- I - I -. - I- -1 1- 1-I I I - I I - - - I -- +-- H

- -l"I I - I I I- 1 00000

10 T '0:1 - 1- 1 I I I -4 -I , I I I I I I -+ I I - I 1- I 1- -100.0( 0

i-Ot. -l i -ff----- I -- i- -I - f - ft{

5B "0: 0 1-. +f,;0 150 22 1 :. 0 300. 00 351. 1 O,. -t -. -:

Azimuth

Page 68: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

-. ',F CS, 1 ST RUN 48. O DEG Si I.I HEAirD l ILTT IISON TIME L~Y HR MIN SEC MILLFPLO.T U R 06 ARIM VS EMNI-STA 2. .3..TIIE 250' FST. PT.IG16 13 10 10 85 Figure 10.14

5 (Design) 6 (Data)

. . 50. 800 100n00 15 08 200. 03 250. 00 3 .00 350. 00 400.00 45:8. 0

50. o - I I I 1 i I I i i I I I- I - --I- -I I- 1 -- I- I _ -I -1 -1 1 I-I-+- - I-- I-I I I -F+-I- - I I I - 500. 0

400.00 - -I I- 1 -- + -t--I- -I +- --- 1- -I --t

H-++--I--I I t I-- -- - I-I I- +-1 --+-+- ---1 - I--I -I 400.03

I 6

300. 0 H---If-I---I----- f--l- -I -- I----I----- - F -----.- . -I- I-I ------------ -- ---I---l--I-H----I--1.- -H-F-- I-.-I--- I-i- 30.00

2. -000 --- 4-I- ! 1 - I---- - I-- - ---- I-L -HH-+ H+I- -' 4-- I--

- - -I- -+I--- -- 3 ~ -1-+- 1"I--- I 200.00

iB-- - 1-- --- --- I t- - - l -I -I--I--I- I -- --- I- --- l-- - l--l- I -l----H - -- --I--1--I- :- -4- -- -I-f- t - - ---- I- 10.09

2-00 00 ti- -I- I I I - -f I I I I --- -I I I -H- --I -- I I--II I - ----- l-+ - I -I-H- -+- I - H-I- I I I-I-- I ---I . ---I -I-- l -I-f-I-I - -- 100.00

±8-0O 00 H- I- I-i-- -Ij.--I- - 1 -- -1 -1- 1- - - ----- I - - 1 - - Il_+ f -- H- -- 1- -I- I -I-I-If_ H--lI--I -I---1-H----- [IH- I-- -f---l-- -f-- H-I--00 8

S I-I III - I-I ,I I I - I- I I I -1- 1 I I I I -- I I I I I i -! -- I I i -I- I II I-I I I-I FI I -i I 2 00

5. 5.0 10. 0 1.50 00 2-. .0.00 3 00 00 550 00 00. 30 4,. 004

Azimuth

Page 69: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

.!'F S I ST RUN 43. 0 DEG hW t IEAlIFI)D .IETTISON TIIE DAY HIR 'II SEC MIII.PLOT Illl:11R 06 A.-ll VS TEII' STA 2S'35.0.TIME 2;'5 FST. PT.016 13 10 10 857 Figure 10.15

5 (Design) 6 (Data)

. ."3 50 0I 100. 1 00 150.00 200 0 250. 00 300. 0 350 00 400. 00 450. 00

500.I0 I- I I - I I - I --II I I --II I I I-IF I I +I-Il -I-- l--II--l-I- -- I -I I : I-I-- - -I-: -I-I-I - 5008 83

" .

S31 0. 00 --1-I-- I--I- I-I---I--- I -- -1 -- I I -I- t - I-I -I-- -II--I-I-+-t'I- . - - t ,-I }- H- --- ---+- 3880.80

0- 000 H i - -I -- --1I- ..00000

50.0058

200. 00 - I --I- I I-I -I l -! l l- l- 1 I ( - - l- l- I - I I f-I- - I--I- ll - -- -l-- - i- I -I - '00.00

0. 0 50 00 1.00. 10 150. 2'1"0 2fi 0 3'0 08 350 u 1 3 ' 0I

Azimuth

Page 70: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

: -' C , I-;T RUN 43. 0 DEG S :.IJ HErAII: .11FTIISON TIME. I IY HIR IIN SEC MILL .

r.; or Nli.', : R 10 A71M VS TEMP'- STA 2t5:'.,TIME 100 FST. PT.016 13 10 10 857 Figure 10.16

9 (Design) A(Data)

So 0.0 50 000 100.00 00 20. 08 250.00 300.00 350. 00 400. oI 450. 00

501.0 -- I I - I I 1- I I ll IH-4- f- I 1 - --f-- II--HI-1 - lI + -1 -4-I1 I1 H -I- I H--11 -+ I- I I 500.0O

400. I- I- I - I - I-- - H - I I I H - I -H--I-- +-- I -I- -.- I-I- -I- - - -I--I -- -I- -- - -- ---- F 4- -- - -+- - - - 400.8

300.8 - -- - ---- -I--I - - 4-4- --+-1 - - -- + --I----+ 4-+-i-- -- -I- - -- I -- 300.00

--2080- F---i-.-I-I-I- I --I--I -I-I - +- -I- I -I- F - I -H-I- -I-I I---------- -- 4- -I--F-I--F--I-- F-I -I--II-I -I--I 288.68

±00800 -- I- I -IIH -+ -- +-- I I- +-+FI I -I I --H- - t++I - -I--I-I -- 1- 1-F-f-H- I--+

.003 0 -- -F--I- l-l- + I-I-F-FII-I I +--I--- -- l- ---- I-l- I-- -I-F.-•

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I--I- - 080.00

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-- I I I - 4 1 I I - I -I I I I---I I- I-I I I i 1 I I iI I I 1- -103 00I

'- " 50.00 100.0 1. *0 22t.) 250 0 200.00 38.03 401-.00 450. 00

Azimuth

Page 71: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SlF S'. i ." RUN -18. 0 DEG SkJ.1 HEAID TIl ISON TIME D'Y HR MIIH SEC MI.L-FLUI HII.;.!; R 10 A-,'I[ VS TEMr' SIA 2b5i?...lIME 150 FST. PT.016 13 10 18 85? Figure 10.17

9 (Design) A (Data)

P';", j3 SO1303 100. 00 15 003 200.00 250.00 300.00-. 5 C00 40. 00O 45'3. 0

500.o 0 F I--II IIII I I I - { IF-I l I I I I- -I I I I I -I -I I i I H l l -

50',00t 'HI IF-I--tF-I- i I t-.I400.80 -- l--I I 1-1-1 - - - 1 F-- fI -iI i - -HI I --- - I I H -- - ---- I-- 1I :---1 -- - 400.00

200. H - i 1-+ 1 I - -t- II -- 1 1- -4- - -+-F - I 1- 300.00

+00.00 ± 1 1-+-41 -4 - 1 :-1 A- 200.0

2. 00 -I-V- -1 -I-- I' -I- I + -1--1- 1- - 4 -t-I--- - -I + -- " -H-- " - - - t -4-+-4 - 2. 00

0 1 ~

20 .0 CI -III-I- I I -1 I - -I-I --f - -- - -I i - I -I -- F -I "----I--I--I --I-- -I---I +I -14- -II- --- I- I-I- I -I- - i---- - --- - -I .

* 10.00r -I-I--II-I- - -I- - I I-I- l-I- -f--I --I - I-I-- I--------- -I-I-- I----I- -l f-- ---- I--I-- I I-- - I--I -I- I -I- -- I- - l-,--I-- f -f-I -I---f-I +--I---l-l--,I - 00.60

-100. 03 -i I I I I H I I I I I I I I I - -- I I I I - - I -- I i+ I- I --I I I-I I I I - -10 .--10.3 *:--, I I-- 1 - -I F 1

I t 2 $ 1i

003 100. no 150. 00 2n1. 3 2 1. 00 300. 1 i -i . o

Azimuth

Page 72: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

F C. 1 ; RUN 13. 0 D[l; SK L .I HEO II L) ,.lTTISON TIlE DAY HR MINl SEC IL..IPLOT IH;:'t R 10 A ,,I VS IEP -STA 2!-b:. .TIME 200 FST. PT.i16 13 1A 10 857 Figure 10.18

s (Design) n (Data)

O '. 00 100. 00 150. 00 200. 00 25. 00 308. 00 350. 00 40. 00 40. 00

500.00 - I 1 1 I I I 1- 1

tI I I- -I-+ -I

1-- I--1 II I I -- -I- -- -- I- -

f II I-I--I-- -- -

I +- tf 1 -I- - H 1 -I--I I I- 500 00

400 00 -t-1 1 I I -H--- I - -1- I---H-1 t -- t-t- -I I F t-+---1 - -- i I--I- I- -I- I ---L-I--I-I 1- 400.00

200. D - I--I-+-1 -4- - --- T- Ii I 4-+--- - I-- H I 1- -- l-- - 1--- l----+----- I-H 4-I-----+ 4-I-I--+ 200.00

S200.03 -I-- -II-F4 ---I- F-1 -+- + I I -+-- " 1 1 -" -" I-+ - F tH -- -- - 4- - - - 10 0.00

- 00040 F t l--I--I- - -I-- -H----- I- -- I- -l--- 4--F-- i- --I - -4 - -- I--I-I- I ------------ I--I-- I--I-+-- --t-- 4- - -- HI-t +- -+ - -- . 00

-100.00 H--I-- I I-- ----- I--I -I----I-- -I --- - - -f-II - + -H - ---- I .-I- - -- 1-4- I --- 4-1- - - ---- I -- I -- I -I 1- -100.00

-2 . 0 I--I I - II I4 I!- I I I -I-I I -I II-1 I -- - I I : I I- I 11 +-I - I- I- I-I- I I I -I-II I i I -20 10i .

-. 3 Brlf 100.00 o 15. f0 230. 03 21;?.08 3 0.0 35. fo -100. it 00

Azimuth

Page 73: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

S:'F C'-, 1 iT RUNI 171. 8 DEG SKL.TI -lE llD JT fISON TIME I~fY HR MIIM SEC MILLFt.Ol iii: R 18 I( ii! VS IEr'- STA 255.. .. TIME 250 FST. PI.016 13 10 180 857 Figure 10.19

Is (Design) (Data)

i- 000 i00 10 150.00 200. i3 2 0. 00 300. 00 350. 00 408. 00 45. 05''. 2 I I I

- I 1 I --I -1 I I --1 1 1 L I- 1- -Il I -1 - i -- - -- I---+- I 1I I - I--I I I I- 5 3.00

40 . - I- I - -I I f I --- 1 1-I-- I - ff +--F- """ 1 1- - ---- --- ---- - 400. 00

• 0 0"" , . .. ' - + - --t" I -- - -- I--4t +, " " -H "I-- - -1-I I- I " + I- 300.0

1000. - f-I- I I-I- -H- -- - --I- --4 -- - - +- -I --F-+- L - --- I--- - --- -- -I---H-1- 1 f I-I-f+ -- 1- 00.00

.00 I -I- 1- -- - I- I- i -I- I ---- - 1 - -- I-- - - -- - -- -+-----I -H 200.100

-14:0. 1 ! - I-- A ' I-1 1 1LH1 I - 1 L--L- ---- I-II--I ----- - I f -f------ 1 --4-0000

-- I-I I I I I - I I I I I I I- - I I I I i I I I I I I I -I-iI I -I I I I - I I I I I i

1- -1013 0 15 0. 00 113 .0i0 200 0 300 00 0 .03i6 l-+l

Page 74: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

F CS :T RUN 48, 8 DEG SI:ElI HETII) JETI ISON TIIME- DfY HR MI SEC MII.LL

FP OT Iti::;: R 10 Z111 VS 1EM:' STA 2552.0.TIE 275 FST. PT.016 13 10 1B 85? Figure 10.20

9(Design) A (Data)

.r- 50. 00j 10.00 150 ie 208.00 250.00 300.00 350.00 400.00 450.00

508o.0U -- I-'I I I -I- - I-I l I I i-----I I I I - {I I- I I : -a -I -I-F I- -I- I 1- I ----- F -F - I- I 1-I-- 1 -I l 4-+---I--I -+-I-I+ I - 50000

408.00 -- I- I-L-I 1---H--I-- ---- --- ---- -I- I --- -- -I--I-I- 1- I-- I--I- - - --- -I--H-1--I-I 4--I- + -- +--- I--I-F 400.00

200. 00 -- H -1 1--- ---- -H- - + 200.0"

10.0 4-- -

- + - - - + 4- + +- -I-- -I--I- CO+--- -. I-- +-- -+A-- 3-8---+ 100.00

-A

.0800 --- - I--I--I t- I - -- I I I-- --I - I -t -- t-- I - I--+--- + I 4 - -I--f -t --- 1--I- -t-- 1--I--I----I-F - -I- 1--+ --- -1-1 -- - -t - -- + --- I -I -t

---H- . 00000

-00. 00 - I I : I -H I -I--I I I-I-I-I - I-Il I-I-I--I I I ------- l--- I 1---- -I-I- I-----I-i-- - - - l- - I I----I- I-l I-I--I -I I II 4-- - 1--F-- I 1-I--b -108. 8

-- z21:n : - 1 I I I I I -I I i I -l I I I 1 -1 -I II I -t -I I l 1 l -- I 1-I I -+ I---- I- I I -I--I -- I I I-Hi I-I I I Il I-I; -; I I I - -2 0. 00

. -.. 5-3. 000. 150 .0 2 00. 2 0. 00 380.00 350 00 -100. n0 4'i,. t0Azimuth

Page 75: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

"I'F CS IST RUM 48. 0 DEG SE-tl HEATED JETTISON TIME DAY HR -MI SEC MILLFLOT IlU:::R 12 ATIM VS EMl '-STA 262.-, TIME 1011 FST. PT.016 13 10 10 857 Figure 10.21

B (Design) c(Data)

0 .. 1 50 0 00 100.08 150.00 200. 00 250. 00 300. 00 350.*00 400.00 450. 00500.00 I-I--I : I I I --- I I i I -I-- I I I I I--I ---t- f- -- - 1- 1 I- -+-I- I I- I ---t 1-I I --- t- ---- I I- 500.00

40.0 -I---I-II i I- t-I 1 -l II +-+-I--f I - I----I + -I- -I-I - - I--I4 - ++ --- I -I --- - -I-I--I--I- --- I- -+-I --- 400.00

c to

±

2 .00 C-+f-41 -1 f1 F I J.+-+---- 14 1-+-I- ---+-I-+-- -- -- 41- 1- - -- H-+----------- - +-- 208.00

10. 00 H-I- -- I-I-1 I- I- - -1 -141-I-I- - --f- - - 1-1-I- - - I-H-I----- -- -l-I -+-- --- I--t- I--I-I I----I-+I---I-+ 1 .0000

00000 1--I- 1 + I--I--1--1----I---- I - -1- -1 +--1--l I I

- + -I-1 - -- --- 1-+ f- I- 1 I- 1- -100.00

-0.00B --- ~l -II-II--I-l-I -II-I -- f- I l-I- l---I-+-I-I-

I I-l- -Il I-I-l l II I- F--I :-I- I-I--I---I II-±- I-I -I- I -100.00

-2I:I.I 0 I-- ~ III III I I I I I 1 f I I I-I I I - 1 I II-20 . 0050. 30 100. 03 153. 00 200. ) 2:'..00 30 350. 0 4 0 4',o. 00

Azimuth

Page 76: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

;T ! LIN RLI:. 8 DIEG S it I HE IEI) it I 15ON T I HE D1iY HR HIN SEC MILL

Rt 12F A. IR 12 IF! VS EIll' SRTA 2 2:T.5" TIME 1513 FST. PT.llG6 13 10 108 b5i Figue 10.22

S(Design) c (Data)

. . u 000 100. 00 150 00 200. 00 250.00 308.08 350.00 400. 00 450.00

50c. l-- I- - I ---- I- I I-I- -- I--I - 1I-I-l ll -I -I-- -I-I--I- I-- I- -- f--F-I- - I-- I I---I-- I--l---II --H -+ I-- I- I 5130.0

400.00 -i- -I-----i I-: I -- ----- I-I 1 -- ------ -I- -H -I I l- --I--f-I- --- I - -I- -I -I- -I---I-- 4-- - -l--Fl- - -4- ---I------I- + -l -I - - -I--- 400.00

E -H-.H 4- -I-0-H-1----l--I-+-I-H--IJ--- 3020.00

. 0 00 ---- l-- I - - I- I--- I- -I- -- --F--F- ---- l--1--- --I--++-- --- -------i---i --F-FH---I- --I----- -- 4- --- -+i-- - 8.00-I -

-71-100. 00 -- l I i I I -1 1 - - 4- I-1i H ----- Il - l I I+ I---- II f-i-- -I-I I- -I- -1- -- I-- I-- -H 4 -!-+- 1-I - - 1-1-1--- 1 -l - -4 00.00

0.3 I-I I i I I I I II : I -I I I : I III I I-II I I I I II I - I-- I- -1--I- I I- I I I I . -I-- I-l- -2f0 0

C - 0.1; 113 100 0 150 000 01000 0 00 0 3 400. 0 4.00

Av mth

Page 77: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

S'FP L.SS 1ST PRUl 13. 0 IEG E tL I-IEl ED JETTISON TIME DAY HR MIN SEC MILL

PIl T Ul-t:i R 12 A0"9-1 VS Ii-i?O STA 267?.'5.TIME 200 FST. PT.016 13 10 10 857 Figure 10.23

P. (Design) c (Data)

Io C, 100 00 150.00 200. 00 25000 300.00 350. 00 40A00 450. 08

5 C00 CO F-I I I I I :- Il i :-- I -II I -- I I I -I I I I li 4- I- -I -l- +- F - I -+ 1 1 I I I -- +-Ill- -I- I - 500.880

400. NO -- - III - I- I - --- I 1 -1--1 - l-I- - 1 - -- I --- ---- f-f - -- -F - I I-I -- - - I --i --+++ I--I 1 - 400.08

0

-00I-

- 11- -I --iI--I I -- -I--- - -- ---I- +- --l -I- - l--t--- --- -i -+--l-l-- -I 300.008

1010.3 -I--I -- 4- -- I -I- - ---l -

--- +-I--I--I I-4----I- -I -I-- --- I--I- - - --- - -f--[- - -- 0 - 4--I -I f-f 1 1 001000013 I--f- 1 I -i ij -4 : -l f F 1 -1 -1++ - 100.00

.IE;B eO I t I ----- I--I- -I I -- 4 -

I- I I -I I I - -F- I - --+ -- - -I I - I 1 I -- F - I 1- .-1 00 0

200.I -- 14 l i l l-l i l -1-l l l ? lI -l- I t- i- " -tt+ I- A I- i l i: f- 11p Fl-o- 02.0 -- II-- I El II-I- -I I -;It I-I -I -+ 1 I II-I II-I I-I- -- F- I I-I--l-- - l--- --I--I-- I- -- I I I-I I I -I0.60

--J00.01 I I I I T -I--I I -100.80G

100.00 1. C ?i30 300. 00 350. 00 0 '1. 00Azimuth

Page 78: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

I' CG IT PUN W.10 0 DEG SI:Ii FILHE t.D .JLTTISON TIME D:IY HR NIN SEC MILLFLOI I I]I;,:-R 12 I.'111M V IEVSI' STA 21;-%.. .IlIIE 250 FST. PT.016 13 18 10 857 Figure 10.24

B (Design) c (Data)

0o'-, s10 oo 1. 00 10.0 150. ( 20.00 250.00 300.00 350.00 400.00 450.00

500. 0 I--i- I I lI : - -: : I -- : I-1 I I H-1- - I- -++i I I-+ -I--1 -fI- +- I + J--I-- -- I- 1 -1 -+ 1 - -i I-1- 500.00

400 - I,------ 1 -- - -I- i -- i -i- -- I-I I- --- -- t----i--- I---I -+'-- - I-- t---I- t'+- F-I--I-i i- f-+- - F -- -+ -I -Ii- -F-- + l-+ - --I ---- i- -I --- I- -- - I- -- 400. 00

300. 00 I'-+-- I "-'--- - --- 4 ---+- - F --l- - --

- +-+-+- + + P- + --- +" -- ----+ --H +--- -I--- 300.0

100.00 --- I--4- --I--- -i-- H--I-- - -+++- -+- --- I +--+-i -- I ---- 1 -I--- F-i--i-I-- -F -1 ----r-+H+- ---- -F-+--- -I- -+-- -- l- 100.00

.00000 -I-i+--F-I--I- I+ -------- ------ -1--- - + +--- I --- l- - 1 +--- +i-I- + 1 - 4--t--H--+ I--- +-I - i 1- .00000

-1 ,08 0C3 : - I I- I I- --I-Ii+-1 I - -I I I -++l-4 I- I - 1- - I --- I' i --I- -- I-- +-I-

-14 -I-t---1 -+ -++ 1--I- """ F- -l "i 1 - -100 00

-2T. "G Ii-Ti I I I I I I I I I i I- I I I I T -I " I I I-'1 -il i i I I I I t- 1+I- I I I I I I I I - -200.00

.00 ,0 100.00 150.00 20 '.10 250.00 300.00 350.08 .100 U0 450.00

Azimuth

Page 79: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

S'F CS, I T.:T RUN 4E. 0 DEG 5-:l.' HiAR1LIi .it l'ISON TIME DAY HR MIIH SEC NIILFl01 OT 'tR 12 OillI M'PTE i'-S T '6.'.iTIME 2/5 FSV. PT.0 16 13 10 10 857 Figure 10.25

8 (Design) c (Data)

. , j; 53. 000 103 0 150. 0e 200. 00 250. 00 300. 00 350.00 400. 00 450. 00

500.00 I-+-1- 1 1 -- I- -I- 1 1 -- 1i I H I I I -- I I i -H -- - I- I - -- I I I I f--- I II -- 5l00r.00

400.00 -1--F-- I- I- - --I- --- I- I -, ----+- H- F -. +---- - 1 -I- -F - I-- -+--- + --l-4-I -t-- -+-- I +-+ 1- I 1 - 1 300.00

E- . 00 t-- --- I - -- 1- l + - + 1 - - 1-I- -I--- +t--t- ----I- ---- - -- i1 -4t-4-t- 1 -I---I- 200. 0

io 0 0 - --- 1-F1 --I I-+1I -- I -i---I- - - -I- F - -1 --- + I- F - - - --f -I- I--- - I--I- I 1 -l+ +-I----H I--- 100.00

+- - i -I- - 1 - H 1 --- 00000

-- 200.0 -- I I -I- --- i I -I i : -1 I - 1 I - l I- -I- I I-I - I -- '1- i- I I -1 r. o00

s5. 00 I;:'. 00 150.0000 0 0 2.1.0 0 300.00 3;50 0i 4o0 .n 4'; I:

Azimuth

Page 80: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

..,T RIJII I:. 0 D -; IFJ II'E1i, .T I lSOII TIIlE DfY FIR MINI SEC MILL

PLO1 II:! :i R 14 0ft(IN VS 1IP -S .TA .. TIME 100 FST. PT.016 13 10 10 857 Figure 10.26

u (Design) E (Data)

.- ." t) r o0 100.00 150 00 2010.00 250.00 300.00 350.00 400. 00 458.. 00

*:0. :.a l-- I : I I - I- I I- -- I-f-f I I -I--If I I I--H .I- I I-I I 'I-f--Il-I-I I f--l--l--f-I-V-I -f--+----- l-lI-I---f--- -i-l- --f- - I I H-.I-- - I I I I- 5C. 0(

400.0 -F--I-I-I I I -1 -t--- . 1 l-F-f- -I I I - - I -+ -1 .- I-- - - 1- 1 1 1: - . + - -+ F- A--- - --f - 1 --.--+ III- 4 .50.00

0)

200 00 -A -I-I - H- -I- I I +- - [f I--I I -t---I I--I-t ---- I-----I-- -F ---- I- - - f--- --- f-I-I-I- - -1-4-+ --I-- H -I--I-- -I-"-- -I--------I- H -I-f- -I---- 20i80. 00

DUB I-(i-f-- -f II 4i- AI-- -1

203. 0 l -I-- -I ---t I 1 -1-1 -F I ,--I -t- + +--I I -I +-I- - i-- -I-H1----+ -I-f- 2I0.I -

.0 0 I--f--I+1 - -I- t- - I -- I-I- - - -ll--f -P - " - -f+ - -+ -- --I I- --+-I-IA- - -I--- -- I--H-- ' I -- I-I-- - H-- -I-I 1000 0

-10ri 1-l- -- I I-- I- F-I- I-I --I--F I - ---- - -l- -I- - I-I f -- - -i -i --- - - I-- - -I-I - I 1 --- ( I -I I- -. 00

0. 0 I I I I I- i I itI I f f I I - I I I I I I I I I I- 1 - II ( - I II -I I - -I I I I--I t1- 1 1- '-

-. .5 0 100.00 850.0 2n ~ ig 250. 00 300.0 50. 00 40.00 4... 03

Page 81: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

S'F CS5 I ST RUN 48, 0 DEG SKEWI, HEAlED JETIISON TIrME DAY HiR MIN SEC MILL

PLOT 4lI,I;:'-R 14 Af 1I VS 1EMIP STA 2723.5.TIME 150 FST. PT.016 13 10 10 857 Figure 10.27

D (Design) E (Data)

. . i 50. 00 100.00 150.00 200.00 250.00 3008. 00 350.00 400 00 4500

400.00 -I-l I - - 1 I--I '- I -- I- I- - -- 1 I -I---+ I- I -I I-I- -I --I - I--I. - ------ I - { - 540000

Foo. -F -iE + + -+-1+ 4 + H-1 --t -I 4i 00. 0

00. 00 - -1 -- 4 -I I I -I- I I-- -I-H-- +- - - +I- -- I-+-I--I- I- Ht - + - 1-- -- 1- -- ++HI-- 4-I--I 2 .00 00

00.00 I- -I-I IF ' - I-- I +-I- -I- F--I-[I-I-4 I I I- - F- -I-I--I I -F--+I --- f -. .I-+++1 1 H -+ - ,H I - - 0.00

-?000 -I I-1 I I I I: - I - I I I I -I I I -I I --- I I I I --- I II I - I-I I : IiI I I 1 -----1 i I--i -IFI!-IF- -I -,I - I I I I : I 1 i --2.00

i000 . oO 150.00 200 :0 0. 00 3 0 400. OAzimuth

Page 82: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SL.: . . r V 'I -3. 0 DEG SKI I HEAlTI) i ll'riS N TINE WilY FIR MIIH SEC rlI L

F: 1If I P 14 F lll1 VS IEP STA 22,.5. TII"F 200 FSTI. PfT..16 13 10 10 857 Figure 10.28

n(Design) E(Data)

50000 100. 00 150 00 208. 00 250. 00 300. 3500 40. 0 450.00

5- .. 1i - . . I'-..I- --- I-1 I-ti I H- I -- --I -- -I- -1 -I I -- H -I- F I -I-----I-I-I I-F.V-J-1-- -I I-I-

5 .0

00 0 - t - I--- I -1 - - 1- 1 t -I---- I- i- - -+- I-I-I -I -1 - I - -- I-. - -i--- + -I - ---I -l- -+-I 4-+ I- 400.00

llI tJ

CLS00.-, -- 1 ------- - H-+ -- -f-f -- +-- t-I-+--'----I- - -- e -f-Ftt--- - -- l--t- --- ---- I-F -- --I I- 3I -- 100.00

i0.000 ,0 4-4--F--+ --I ......H1 + -1 4 -- + - i.0001 1-1 +-+-i- VI I-I -I 4-4--1--4- t-

-1 r00.o0 ++i -1 1 1---1 - I + I I - I - I-- - 1-t-- -

I-- -1-4- ++ -- --+-- - ... . .H--- - t 4 -t4 I-- ----- + -t --- -H- -- -I-.i -i 00.09

L - -I

- I200.0 - 1 I-I -I I 1 I -1-1 1 I I - .- 1 1 I--l I- - I-I --I-I-I --I - - I-I- -- I- -I-- -I---I I--t I -I 1 - 00.00-?--I-l- 1 1I C- 4 I -I-I I - + I I- -I--I-I -I-I-I ti

5) 00.0 50 0 20 0.( 250,0 300.00 350.00 400, e A 2 00

Az ituth

Page 83: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

S'F C.,S ibT RUN 48. 8 DEG S1,1k HE-IED JETTISN TIME DAY HR MIN SEC MILL

PLOT Hi: R 14 71H VS TEIH- STA 22;;.5,TIIIE 251 FST. PT.0I16 13 18 857 Figure 10.29D (Design) E (Data)

.c0 50. 000 100. 00 150. 0 200.00 250.00 200.00 350.00 400.00 450. 0

5010.00 +--4 - I -I -I----I -I- I 1---- II I I -+-I I ---1--I -- H -I--I I - -- -I-I-I -- --- I- I- H - - I I-I--I- I. H+1 I-I I 1- 500.00

400.03 - - -- 1- H++-+-I- I--i- I - - I--I-I--I-+ -I-I-I+--I--I-I- -l- ---- l-- --- i - -

t -- f++ -- I- - 400.00

2008. --- I-+- --- -- -- I - -I-1---4--0 0-I-+.--IH--I -I -- i-- -- --I--I--I -I-I- ---- I-- --F--- --f----- - 300.0MIa

S" 303 91-mt-.- -- +- + -Hi+-1 f----+t ----- - 00.

200.00 4-- -I -I 4-- f-- I--I- -t- I-I -+- --1f I --f + -- I-" -I----- -+ - - - - I- 4 ---I- I- -- 200.00

000013 0 --- I-I- I -f1- -f-- 1 -- -1- -1- ----- ----I- - - 1- I- -I---- -I-----I--I-- t 1--I-- 4-I I -- - - -- .00000

-10 I -- II I- I- - I- I-I I I--I+- -- I- -I I-4-I- 1 H -- Il -1I----- 1- 1 + - I- I -- 4-t-- 1 -- I -I-H-- I l-I-I I 1- -100.00

-20 0 I ".3 I I -l - I I I-I- IT I I -- I I- I I I I I -I-I I I-I- I I- -t--I -I I I- -l I I I -20t] P0

G. 00 130.0 1.50.0 20r n0.0 -300.0c 350. .0no0 0 3n

Page 84: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

S ';T RUM 'S1.. 0 DEG SKI I en II : .JI-TI SO N "I E DY HR -II SEC MILL.1- .::;:-R 14 AI I VS LW STA I2..5.TIME 2/' FSI. PT.016 13 10 10 857 Figure 10.30

D (Design) E (Data)

,.-f 00 10000 150.0 2.0 2210.00 300 00 350.00 400.00 45;. 00

i00 00 -- I- I i I -I I I- -i- I-I I I-F -I - -- --- I-+- I--I-I -I I + I --I 50300

6 41-1 -IF 1. IA-+-t- 1 - +-- +A- 300. 0

EE E

E E

100. 0 --- I-I -I--II ---- I- I-I-I I- - -- I - I- -- I I -H -- - I - I- I I- - - I -I --l -I- - I-- -I-- I-I--+- f-- I 1 -- 4 - 1 1- +- 2 . 00

100. 1 --H-I--1 1 1 - F- -II I-t-I +H IH .00000

0000 ---- - - I -1 4 - 1 - - 1-111

--2 1 It IIII II- II -- I I I I- I I I I-- I -I - I -I-1 -I-I I 0 0 -1--f- (I- I I .--I-I- I- 1 1-~-- I -I-I I I-I- I I I -- I I I -- 7 00

- r" -.. s. 00B 10'.00 150.0 200.l0 25-'. 00 0000 350. 00 40j 1 '.0 00

Page 85: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SPF CSS--Ib-T RUHI. 0 DEG SI-FIJ HElEn. JETTISOn TIMNE DOY FIR NIH SEC MILL

PLOT NHiiNR 16 Aii VS tEMPt STAF 272.O.,TIME 100 FST. PT.016 13 10 10 65? Figure 10.31

F (Design) c (Data)

cOL_ 50. 00 100. 0 .5 00 200.00 250.00 300.00 350. 00 400.00 45:'. 0

500 - -F- II - I I I- - I I -F-F-I -I-- I -- i---I-I -I I -I-- - - --1I---- F-I-I I- - -. t-4 -- 5011. 00

4 F.00 I I- I- I - -I- - i- I + - 1 I-+-H+-++1--- I- - -- I--I-I- I I-- -- l- --- I l--1---- l -1-+- -- I H-+-1 - i - 400.0

30000 -- f--- --I4 f - ---- I -+ -i - - +-- I-4I I- - -- H-I----I- - +-I- I- 4 -I--+-+ ---- i-41

- 300.00

+ + I

-2--. F00- +- - I -

-I - - I- -F-I- + - --I---I-- -1 1 -- I---I - +--I- ----- I-I-I - -+ +-I-- - -+-I--- -+-+--2-I00. 0OFFFFFFF1.FFI-F}FFFTFFFF IFFFFFI 01(FIfF -f jOOFG FF F OF tWF- ifFT ER If

--0000 - I- I. I I I I . + -- -+ + - H I- --- +-. -- - I + +I----- .I I I --I - ---I- -. - + -- - l- - I- I I .0 .00

--200 n"; \ |I I I !i I , , I i Itt-l i l H i l-i l l i i I T ( I I- I I -I I , - I -I I- 01

t5i: rTIO ICUnO IIn nr 200. '.i. 00 300. 0 350 0 4. -1 .00

Azirruth

Page 86: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

:'F CS:., I'1T RLIN 41. 0 DEG 51AI- i HEAlll) JlTI SON TIME IDiY HR NtI SEC MILL

PLOT n-: ;i;':R 16 A Zl VS [ti'i STA 292.0,TIME 150 FST. PT.016 13 10 10 857 Figure 10.32

F (Design) c (Data)

05. 0500 100.00 150.00 280.00 250.00 308.00 350.00 400. 00 450. 0

50 0 1 I-I---I I -I II- -I I-I - II- + I (- I -- l--I I- H-l II- - -I I --- - 1 1 H -- - I I ---H-+- I ' - 503. 00

400. 00 I I- 1-- -II- II- +- 1 -i f -- t+--+ -t f-I--I--I--I--I-- I-I--I--If -I-f-44 --- I--- 4- -I-I-+ +--- I ---I-- I-4--I-+-+- -I---4--I I--+-- F - --I----- I--I I - 400. 08

0108 4 ,00 f-I- l i--- - - -+f-+- l -- H -tH + -- -+ 20--H-+ -+---- -- i- I - -- -1- -+ i . 0

.00-000 (-rr fI- I -- + I-+TI-t fI-I It I H -I-++ I -HH H ---I--I-4--l-- 1 -HI--II----I-l -H-4I-'-I----F- -t-+4- - .0008

.0o. 00 - 4-11 -I I li 4II -1-1- - - 4-+4-4- H + 1 -H+++ + H+ - 1-0+4- If---+-4 -++- t-00

r I--M20. 0 --- I- - II I ' -- I I -I- - -I-I- 1 1-- -- I - I - I -- I-I--I -- - I II -- !--1-4-1- -. -- i- --.--I- ---- -+ -~ l -t I -I--I1 -I ' I-

q -100.80

-20. . :-I I : II I I -- I I I I-IPl I-I I-I------I-II I I H I --- l-I-I- -I I-I-I I1- -I-I-I-l- I--1-1-1-- - l-- I--I--l-I-I- I I--I-I-I I -I- II I I I i--2100 00

501100. C3 18 150. 00 200. 00 250.00 3080.0 350. ( 100. 00 t;l0. 00

Azimuth

Page 87: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

F CSS [ST RUN 48. 0 DEG S.EI. HEWlED JI11TISON TIME DALY HR MI SEC MILL

PLOT HUVFiI-R 16 -1 1fl VS JTis' STA 2792.f.TIME 200f FST. PT.016 13 18D 16 85; Figure 10.33

r (Design) c (Data)

0. I:i 50s e 10,.0 150.00 200O. 2 '50.0 300. 61 350. 00 4000. 0 4508.50 0 -}+-1 1 -0 1 -+ 1 I I 4 -- + 1 l500.00 [I-Yf -1 l f I- I- 1- I -I- Iii H- - I I -- I i i -l.-I- i -l-+ -- 4-- l |- I 1-I-I--- I -I1 - 400.00

400. 00 - 1---I- I -1 -I- -I I +--+ -I -- --- - + 1 +-I- -I--- ,---I-- I- F--- --+ I-F- I . . I I i -- + I -:- -!-- I - 400.00

300. 00 -- 4-+ F----,- I-- -- f --i - +I -+- -I --l +f--+-I +--- T- IF -I--I --- ---- +-I --- I-- -f-f-- 4 -- .- - 1--I- - I -- - I- +- -I- " -I --+1- - 300. 00

-G

2.60 --+----I- -- --i- --- I- I --- I -l- tI-t--t--t+ --I4-i - I-- t ---f---I--" - -I--f- - t- +--I--1l-- - t-I--- ---- -+ - ------- I-- -- 1-- --I--I---t It-t+- - -- I- + -I 26. 8

100.00 I"-- -'-t -I- --- +-+ --- -. II -.----- ------t-f + H + t-- +-- - -- H -- -- +- - 100.00

000-06 - - i I-I-- -- I-- F- +-t- -i--1 -- I +----H--l- I-f-I-t--l-----I-i H----I-I- I - -I- -f+-I--I---- I-----H-H- + I I - - I --i---l- :-i- 1---- .00100

-100.CO --- -- I I I -- I- i - -I-I-- I -+ I I I--+--I---I I -I- -- I- - I - I I I -- I -- -I-F - - -1--- l------- I -I--I-- - I I ---- i I -1 1 - -i0.o00

- .I. t i I I I I i I- I -I I I I I - I I I I I I -l-- 03 00I .t_. 00 iu0 15

1 0)0 21--0.10 _.0. 00 h.CI 3 0.0 1C., "1.0

Azimuth

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'vF uC RIN I. 0 DEG. ' -0.DII l HERIIHt .IETIrISuN TIME JnY HR NIN SEC MII.L

Plir tI: R 16 ri: VS t-ll' STA 2?92.O,TIME 250 FST. PT.016 13 10 10 857 Figure 10.34F (Design) c (Data)

: 3,. ~0o 100. 0 150. 0o 200. 00 250.00 308. 00 0.00 400.00 450.00

500.03 i-I I F I I- I HI I -II-: --- -I- I -H -I I i---H ++-1- I-I - -I- +-I- I +--- H +i- - . --- --- I -H-- --- I- - I--F 500. 00

400.00 +-+-I- -+ I - -+- -- I-I -I- I----+ - -I +--- - -I-H l-- -+ -4 V -++ --- I t-- -H--I-I-- 1- -- I-I-+-++-- I4--- -- I-- + 4-I--4 40. 00

"FrFF

.FF

3100.03 -•--- H + -I --4-t- -H--- H -V-- 4- '+

- 100.00

-00 0- I-III-I-II - ll-I-I -- I- I I I -I -H-- I-i I -- 1---I1-- I Il- i- I IFl-- iI- -- I-I-F I i i -I - I I -- 400.00

0 50.000 100.3 150.00 200. O0O 25000 30.00 35000 400.00 15'. 00An010+0

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!'t- CS' I ST -RUN 48, B DEG SKI:J HEIILD JETTISCH TIME DAY HR 1I114 SEC MILL

P1 01T NI:i" ::R 16 A* III VS 1EMFP STA 2.92..TIME 275 FST. PT.FIl6 13 10 10 857 Figure 10.35

F(Design) c (Data)

o0;: 50. 000 100.00 15o. 00 200.00 20o. 00 3008.00 350.00 400.00 450.00

500.00 eo I--t- I i -- I f -i I H I I I-I : 1 1-1-1 -1 : 1 --- - I 1 - I- I- I -- I I -H -I" HI I - H -- I-- I -- -I I 1- 500.00

490.00 - -- --- -I ! - -i I -t- - t +- --- - t -- F t- - + -+- -F +---' - (-- --- + }- +-I- -I-- I--I- 408.08

FFFF FFFFFF

v 300.00 f---f1-- --- --- -1-+- -- f-I-+ -- -'--1- -H+- + -- '+ i +t---- t -1 308.88

200- r00 - -++ -t- +1--H- f1- -+-+- + - --- H--+ - 4-1-H-I -+--- -- - H-H-1- +- + 1-t--4-1- -F---+-- 200.00-

100. 00 -I+-H- -- f A- H-+--++-+ ++ H+-t++ --ft -- -1 ---- + - 1O. 00

- 20 00 -I-- 1-- I---1 l I--I--I--I- -- - t-- I--I--+ + --I-----I + + ---- I---- - 1-- 1-1------ -I4- ---+- -- I-H--H - ----- I--I- - 2008800

-10 00 - -- I I-I I I -I I I- - I I 1--1 - 4 I- I -I- : I-I- :' -I i -1 I -I I--I--I- I--I -- 11--4--I- I- F-I-- --- I I i H - I -- -- I-- -80.00

-0 00- -f-vJ I- I ',I I I I i - fI-I I I I -- I- - I I I -I--I P I--I- I _ -I -I -- I--I I I-I--l -I I I--f--I I I i -- i- 11 -- I--I-II I--I -I -4 . 08

' 5. 000 100. 00 i 20313 20.0 0 300 35130.10 -300 P.. I

Azimuth

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. F .C. -:: ; RUN :10, 8 DIG SK l HERI 0 Jl [[SON TIIME I,.YP HR ' IIH SEC MIL36

PLOT NIl::: :.R 18 071? VS IEMP STA 2R:2fl.-,TIME 100 FST. PT.016 13 10 10 857 Figure 10.36

H (Design) I (Data)C : 5. 000 100.00 15. 00 20088.00 250.00 300.00 3508.00 400.00 450.00

5 e. :-I t 1 i I F- 1 : I i - 1- 1 F - -I I -I - i I 1--l- I- I -- --- ---- - 1- --i-i--1 I - -1 1 1 --- 500.00I i-I-'-l----"I-j I -I- H --- ' . 58000

400 -I- -I I I -- I---I- I--IH - I - t--- " I-H 4-- -+ -- -- -+- i---H--I-I-- f- - 1 -4-I--1-H+ --I +-- -1 --. 400.00

.'- 8 0 --400 -- +- 1-I -i--I--I - ---- 4- -I --i- i +--- -H- IH- - -f -,- +-H+HH I- i--H -V--I- -- 308.00

4 1 I44i44 i-H-++- pp- qpi- -Hf -+H +- 2He

200.00 I --l4 I l-I I --t-t-' t -I -+ 'J--F--H - + 4 H- 2F--00 00

0000 ---- --- f - - I- H : --- -I -- I-- - I- I - ------- - -I--- - '--4- -- i-i4 -

- ---I- H- -i -I--- 1- .0000

00g-o -- I- --- I 1-4 -I-i --l-- ---I-b --4-+- 4--I- I--I---H- -I H - ------ I- I--I- -I-- H +- --- I - I- -i i----i- I - H-+- I- I-l- +- .00088

100. -I- I - I I-t I I I-- -1-1-4 - - I I I - -1 H + t

1 1 -1- - I -I I +- +-1- I - + - I - --f -I -I-- -I - --- t-I I- -- I- - H-- - 1-- I - 100.00

-2 0 I I I I I I I I -H - I 1I I I iI I I I-I -- I I-i-I I I -I I I I I I I --I I -- 00

r:E. 800 ton. 08 15.0o 200. 00 250. 00 30.00 35a 00 100300 ,150.0.O

Azinuth

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SIF C', 1t T RUN 48, 0 DEG SKE-L HEA LED JETTISON TIfIE DAY HR MIN SEC MILLPLO.T t!';I:I.R 18 AZlM VS TEMIP--STA 2820.0,,TIME 150 FST. PT.016 13 10 18 857 Figure 10.37

N (Design) 1 (Data)

S50l. 000 100.00 150.0 200.00 250.08 308.08 35.00 480.00 450.00500 £ H I- I t +-- - I I- H--- I-+ -- --- I I - -I I -I-I- - I- I--A -- - -- I +--- - I ---- - i -I - - l--4-I- - - 0.0

400. C +--f- I---.-l-4 1- --I-- - -I-I- - I 1- - --I-- f+ f -I- I- f +1-1--I- -- ----- I- -I -1- + --F- -- -+- -I- -- 400.00

200.00 -- 4+-1-4-- - 1-+ -- + - - -+ - H-+- ++-- + + - - -H-H- + - l-- -F - 4+-4- 2 8800.

.00 3 - - - - ---- F 4---f +-- - 4 4 { -44 H-4f-I -- I-+ -I-- +- + -I-+ I - I i+4-1-+ 1- -1 +H- ---- I--I .0000

-00.003 -++I----I- I -I + -- -I - I-- fI----•

-- -1 -1-1 1 -)-I - - I-+- 4--- I - --- I -- -I -- I H-- I- I-I I- -l 00 00

- -I I t i -I t I V 1 1 1 -1 1I , I -I- I I ---4 -II 1 I+ - I .I -I - I I I I I : -f -2I 00

S50 000 1O. 00 150 03 20i6 2..09 300. o 350 0L -03 0 01.08htq ,-n+h

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SIm'F CL' . '.T RUN .18. 0 DEG SKI IIL 0 JEI-TTISON TItE iAY HR MII SEC MII.--

PI.1I I 41;,.:;:R 18 Atl VS TlrMI' STA 2 f' .tTIME 200 FST. PT.016 13 10 10 85? Figure 10.38

w (Design) i (Data)

50. 800 100. 00 150. 00 200.00 250.00 300.00 50.00 400.00 450.0

50 -91--.: : -4-- IlI - - --- H- -- H --- I 4 --- I- I -- - - I -- I H - I -4- -1--- - -H - 1- I I-I 500.00

400. -- - - f---I-- I V- 1 I +- -+-- f-f - I -- ++ -- f -1 H -- 1- +- - +1-- 1-1- 400.0- -

a I200.00 I .- ---- --- 1-- +f-H-I i .. --I--- t-- -4+ - t- +- H-4l--f - H-+4-It- -f 320.00

100.0 - t--1--I- I - f--f --I--- - I- {- - -I-- t---f-t- +-- H- - 1 00.80

-0000 -±-4 -+- -I.--I-- -1-4--+-----i-- -- f--------+--+ -- I-----------H- I- - -1 t------- -I1- .00000

-100.00 - -1-t 1 1- --- 1--- I 44-A - - - +11- I - 1

I---- I I-1 - 1-f- - - 1- - --1 -- -I-+1- t--l -- 1 - I---I--+-- 1 -1 -4- 1 -I -100.00-10..0 -- I-I-------I- I-I- ----- I-I--f'I- -I -I-- I -4- I A-f--I--I -I---f---f--f--f---A- f-F-ff-l-I -f -I- -- I---------I--H- --- I---I--f -- -I-I--I--f-----I-f--l - -I--I -I-I I- I -I - -100.00

f-2f: -I - I-I I ll - -I I III-f -- f 1 1 1- I1- 1 I I- I- -- I- - -I I Il HI-I - -1- I I -I - I II- I I ~ 2 00

5r: 0. 5 000 10. 00 0 50. (10 200. 10 250. 00 300. 00 350 00 100. 0 45Q. 00

Azimuth

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SPF CSS IST RUN I8, 0 DEG SKEI HE 1nErD JETTISON TIME DAY HFR MIH SEC MILLPLOT NKI::FR 18 AlIM VS 1EIiP -STA 2820:C,TIMIE 250 FST. P.016 13 10 10 857 Figure 10.39

w (Design) 1 (Data)

ci.:ti 50. 000 ir0. 00 1500 200.00 250.00 300.00 350.00 40000 450.00

500.3 -- -I I I- l I I HI I -4- I I iA- -I-- I-- H - I - i-1-lI- I -- II- - 4 - --+4--- I 500.0

4 0 0 .- - I --.I-I- --- - - - - I

-

.- --- I -- I I -A -- I- -1 I-- -- --f---+-1- - .-- - - -- -

I I200. I I - - t-F I -- 4 II--F- - - I-1f ,FH - - - I- - - I H-1- I H- I -100.00

1 200.00 - t I-- l --- -I-+- ---- I--- -- 4- ----I-I----+-+ --I+i- -I- 200.00

. -F----+-++-F+'-I + 00

.000 -iI----I--F- l -I -I- -f--I-- I--IF- --- - I I I-I--l--I-- - I-I -H--I--F I-i ------- -I I--f-- -- -I- "I---I---F F- -- I -- I-- I -I--I-I-'-I. F-I l 00000

-400.00 I- -fl I I I -- 1 I ! - + - 11 1 1 I I----I-4

-I I I :-------I-I -I -I-I-I - I--. -- j - I --- 1- 1 - l-: 1 1 1 1- - -100.00

I-i I i II- - -I I 1-I I I I I I I I I i 1 1-I : :-I - I I --20.00

."" 000 10 00 1500 0 2',1. 00 300.00 35000 100. C ,-I 004 rl, .

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'I- CS I T RUIN 'I. E Df f SI I FA I I 1Cl T . II11SOI T IME DAIY HR MNI SEC MilL.

FL0F I' .R 18 I;')M VS IE.I;' STA 28.I.-I.1.TIME 2r's FST. PT.016 13 1 16 857 Figure 10.40

t (Design) -(Data)

c 0 51. 00 100. 00 15. 00 200. 00 250.800 30. 0 350.00 400 80 450.00

500.0 I I - I I I -I--I I -I I I 1 1 1-I -H I - I - I- I I- -- I I-H I- I-I--- --- i-- I--I-- I I-H-I-I-I I I I----I-- I- I H 500.00

480.00 H 1- -1 - -- I I -: 4-l-- I- - 1--I-I I-I- II ----+ -- i +-I--i --- I--I - - I-I-+-++I-- 4-4---I - -t - I-I-- 400.0

I1

200. 08 4-+-f--4--f I +- - -I- I- I -I-+-+--- I--I -- -- t -- -- + I-- - -- +-l --- + - --++4-H-- I-I---l-1--l-l -- +- -l--- -- 1200. 00

183 00 8 -- H-- I- 1 -I I- -- t 1- -- i- I-I- iI ------ - - -+ ---I- I- -- -I- -- I--+ ----- I- -t -I- - l- I - -- - -- I---I--I--I -I 00. 00

.l00.00 -i-I -I--I-1i 1 I - -1- I I -- l-I - -- I--I - -I- I - ---H-- + I +-I- -I I-- -I-I------ -- I- -- +1- -H- 1-i H - I- 1- -- - .000-

-00. 0 +-+I-iI I -1 - II I-I-- -4 P - I I - -H I -- - II I-- A-- -I --I-+- -I- + I-I- -- ----I-- - -- ------ I- - I I -- I-- - -I - -I-- -1 80. 8O

P 0 . 0 1-_1 I -I : 1- 1 -- I I- III I 1- -200 00

.0 l.3 51 100 . 0 158. 03 200.10 250.00 300.0 350.00 0. 0 400 0

Azimuth

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Figures 11.1 thru 11.15.

Circumferential deflection and design

temperature distributions.

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SPF CSS-FST RUN 43. 0 DEG StI(EJ HJT, TIME 100 SEC TIME DAY HR MIN SEC MILL

PLOT NUMEER 04 AZIM VS DEFLXIOO,D TEMP-STA 2377 FST. PT.016 13 18 16 857 Figure 11.1

3 Dsiln 4 Deflection

00C00 50. 000 100. 00 15e. 0 200. 88 250. 88 30066. 88 35. 6 400. 6 450.00

-*4r

. . . . . . . . . . .. . . . . . , . . . . . , , .. . . . , , . .

C,

-i 108 80 . . . . . . . . .' : ', : 'I I i0.. 0

S4- 4 4. 44 4 4

*-44

-10 0. ' ' i i ' ' ' ' ' ' ' ' . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .i. .i.. . . . . -ioa. .0

0000 50.00 10.00 150.03 200.06 250.00 320.00 353.00 400 00 450. 0

Azimuth

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SPF CSS-FST RUN 48. 0 DEG SKEI HJT. TIME 158 SEC TIME DAFY HR MIN SEC MILL

PLOT NUMBER 04 AZIM VS DEFLX100,D TEMP-STA 2377 FST. PT.016 13 18 18 857 Figure 11.2

Design 4 Deflectiontemp.000000 58.0 00.0 8 150.80 200.88 256.88 388. 358. 488. B0 45. 8

(5

0

-200. 0 I I . . . , . . . . . . . . , . . . . .. . .• ,

$,4

-4.1-1--1-1-1--1- ±081I 88

000 5. 0. 00 5. 200 250.00 30.00 350.00 4000 40.

-Azimuth

.soooo 53.808 108.08 ±50. 08 20. 0 258.08 3o0.00 58.08 400.09 4s0.00Azimuth

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SPF CSS-FST RUN 48. 0 DEG SKEU HJT. TIME 206 SEC TIME DAY HR MIN SEC MILL

PLOT NUMBER 04 AZIM VS DEFLXIOO.D TEMP-STA 2377 FST. PT.016 13 IB 10 857 Figure 11.3Design 4 Deflectiontemp.

. 00Bee 58. 00 100. 08 158. o 209. 0 25. 0088 300. 0 35. 400.8800 450. 09

488. 80 -+-+-t--9-+-i- I-- I 4 4 4 -3m.-- - - - - - + - - - - + + - - - -lalI 8

210 .03 , I I . . . . . . ... .. . . '. . . . . . . . . . . I . . . . . . . . . . . . . . . . .. ' ' ' ' ' ' ' ' ' ' ' ' ' ' in .0.

0r r

0)

.A00130 53. 000 100. @a 15e. 00 200. M8 250. 00 300. no 350.03 400. 00 450. 03

0 ~ -jgj .e . . . . . , . . . . . , . . . . . . . . . . . . . , . . . . . . . . . . . . . . . . ,_0 .e

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SPF CSS-FST RUN 48, 0 DEG SKEU HJT. TIME 258 SEC TIME DAY HR MIN SEC MILL

PLOT NUMBER 84 AZIM VS DEFLX108.D TEMP-STA 2377 FST. PT.016 13 18 18 857 Figure 11.43 Design 4 Deflection

temp..00000 50.000 100.00 150.00 208. 0 250.08 300.00 350.00 400.00 450.00

500.00 i" iiiiiii 0i iiii ii fi. ... ... I ;l ii 1 i II,, I1'; '" ' . ... .. ........

400.00 1i i i f i i i i H 1, 1 1 ,1 1, . . .I.I.I.I1 f 1 400 .00

400.0 ii i i l I l I ' ' i I I I I I I I I I

1 I ', I , I i

" : 00 0

0.

0

200.00 1 . .± 3200.00

.6.... ' ' ' ....................... 00

8

4 44

00 0 I 4 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 00 0+ -- +- 4 .(3l .0000

0

.0000J 50.00G 00. 08 150. 0 200.00 250.00 300.00 350.08 400.00 450. 00

Azimuth

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SPF CSS-FST RUN48, B DEG SKEW HJT. TIME 275 SEC TIME DAY HR MIN SEC MILL

PLOT NUMBER 84 AZIM VS DEFLXIOB,D TEMP-STA 2377 FST. PT.016 13 10 10 857 Figure 11.53 Design 4 Deflection

temp.

. 000 50. 600 10B. 00 150.00 200.00 250.00 300. 00 350.00 400. 60 450.00

H00 .0 0 . . . . . .H . H 2 9 . 6

4 4

4 4 4 4

0*4

CS . . . . . . . . .. . . . . . . .0. . . . . . . .4 1 I I . . . . . . . . . '. - ' ' ''"" 0 .000.0 0

-- 00. c-aII+IIII -It--I--4--I- . -- + 4-- -200. 08

S 5. 800 10.008 15.08 20.00 250.0 0. 00 350. 00 400. 00 45. 00- -Azimuth

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SPF CSS-FST RUN 48. B DEG SKEW HJT, TIME 188 SEC TIME DAY HR MIN SEC MILL*

PLOT NUrBER 06 AZIM VS DEFLXIB.,D TEMFP-STA 2459 FST. PT.016 13 10 18 857 Figure 11.6

5 Design 6 Deflectiontemp.

.00000 50. 800 i0. 0 50.88 20. 06 258.00 380.88 358.00 400.00 450.08

400. 00 i 1 I I I I i I I I .I . . .I . I I 400.0

400.00 -ili---+ I-1 11-.--F--t-1 -I+-I4--I-F--I4 -H-1----III -I-I-4-+I-+--I-I H-I-H-I--H--HF--I-+i 11 11 -I-$--H-----F +---4+----I -4---I-4--- +--H- t 4200, S6

8.

- i ,."." ...... ...... . ........

. . . . . . . . . ..6

) 6

6-

"0 .L l I II ti . . . . . . . . . . . . . .r.I 6

0 6

(D

-2-0.00 -1- 4--- -- 4- -4-I--L-4-- - --4-F f 4- -H--I--+I-I--+ 4±-- ---- + -I0-I---I-- +- - -H--I-------+-- -I-------I--+--I- ---- I---I-I--I--- -08.0

. 50 00 i00.00 150.0 200.00 250.00 30. o0 350.08 4680.00 450.800

Azimuth

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SPF CSS-FST RUN 48, 8 DEG SKEW HJT, TIME 150 SEC TIME DAY HR MIN SEC MILLPLOT NUMBER 06 AZIM VS DEFLXIOB,D TEMP-STA 2459 FST. PT.016 13 18 18 857 Figure 11.7

s Design £ Deflectiontemp.

.0000 50. 0008 i. 88 150. 08 208.80 250. 08 300. 00 35. 80 40. O 450.08

Soo. U CIO i l. . . .l.l. 500.00

480.8 00. H F * + S i + -i . . -H I IIII - -l- + I - i i -I---- 1, , , , 48600.008

i f

*66a6

0

-2 00 .... ' " ' ' - " L . .... ' t ' ' ' ' ' -J '-' -200 O0

. B 0 50. 0.0 150. 00 200.08 250.0 300.08 350. 00O 408.00 45.00A .i mI t.h

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SPF CSS-FST RUN 48, B DEG SKEW HJT, TIME 280 SEC TIME DAY HR MIN SEC MILL

PLOT NUMBER 06 AZIM VS DEFLXIB0.D TEMP-STA 2459 FST. PT.016 13 18 10 857 Figure 11.8

SDesign 6 Deflectiontemp.

0000 50. 88 100 008 15. 00 28. 00 250.08 300. 00 350.00 400.00 458. e8

580. 0l H im H III I I I I fI ...

sa-............ 390.00

,.4

390.00 i l l l i lili l i l l

w4U

S5.. . .. .. . .. .. 4 . Be

0.00 . . .

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SPF CSS-FST RUN 48, 0 DEG SKEI HJT, TIME 250 SEC TIME DAY HR MIN SEC MILL

PLOT NUMPBER 06 AZIM VS DEFLXI00.D TEMP-STA 2459 FST. PT.016 13 10 10 857 Figure 11.9

5 Design c Deflectiontemp.

e WOOe 50. 00 1i0B. 150. 0 200.00 250.00 08.00 350. BE 400.00 450.00

3m . 08 -+ e i . . . . . . . . .i . i : i ; ,.. 00

E- 200 N i +++++ + -+i i-t- i -I-i l + - -i 4-4-1- 4- 203.00

- " i i l i .l I Ii Ii il l

a

r,4

0 6 . ..00

0

088 0 ±.88 ±50 8.0 289.00 258.08 00 03 250 00 400.00 450.08

Page 105: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SPF CSS-FST RUN 48, 0 DEG SKEt HJT, TIME 275 SEC TIME DAY HR MIN SEC MILL

PLOT NUMBER 06 AZIM VS DEFLXIOO,D TEMIP-STA 2459 FST. PT.016 13 10 10 857 Figure 1l.10

5 Design 6 Deflectiontemp.

5O0 .O 50. 000 10.00 50.00 200.00 250.00 300.00 350.80 480.08 450.00I .Ii I Il- .I 1 4fl " "0"."

50.00

r-I

0

. . ... . ,. .. . . . . . .

• -1D0. e? ------------- ------- -I--4----I--I----- -.---- I--+-I--I--- -j--c----4----e- -I- --- --f------.4 - I- - - -+--- -f---- -- I - -I--I-+--------I- -200 e

0. -00 50. f 100.04 158. 1 200.0 0 250.00 300. O 30.0 4 00.00 450. 00

Azimuth

Page 106: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SPF CSS-FST RUN 48, 0 DEG SKEU HJT, TIME 100 SEC TItE DAY HR MIN SEC MILL

PLOT NUMBER 12 AZIM VS DEFLX100,D TEMP,-STA 2664 FST. PT.016 13 10 10 857 Figure 11.31

B Design c Deflectiontemp.

0.3000 50. 000 1e. 00 15 .00 200.00 250. 00 300. 00 350. 00 480.00 450.00

408.00 .-..+. 1+-+.+- + + H - I.-... ,-.-I.iii. - . i.- 500.00

--

S400..00 - . . .-t-- - - -+- I I II - - .II .

0 00.16

8

4C C

- - C C C

10 0

4

H

-2E0.00 -- .. I4- -I .... ...... H H -f -- -- -'20, 00

S00 8 50.000 100.00 150 0 200.00 250.00 300. 0 "350.00 400.00 450.00

Azimuth

Page 107: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SPF CSS-FST RUN 48. 0 DEG SKEW HJT. TIME- 150 SEC TIME DAY HR MIN SEC MILL

PLOT NUMBER 12 AZIM VS DEFLX100,D TEMP-STA 2664 FST. PT.016 13 10 10 857 Figure 11.12

B Design c Deflectiontemp.

000 50.000 100. 00 150 00 200.00 258.00 300.00 350.00 400.00 450.00

400. 0 - ++ + - 4- -. ... . .. ... 40.00

0

300.08 1 11- - I1 ---, -.. ... 300.0

C C C C

T' 2.80800 k I ''t .I I I! I ; ; " I I I I I I I..

280 88 -4- t..-. . . .. . . . . . . . .-.......... 'I I - I-- 200. 00

-C C

, C

.00s00 58.000 0o.00o 50. 0 208.00 250.00 30r.08 350.00 400. O0 4'0. 00

Azimuth

Page 108: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SPF CSS-FST RUN 48, 8 DEG SKEW HJT. TIME 2088 SEC TIME DAY HR MIN SEC MILLPLOT NUMBER 12 AZIM VS DEFLX100,D TEMP-STA 2664 FST. PT.016 13 10 10 857 Figure 11.13

s Design c Deflectiontemp.

.00000 50. 000 100.00 150.00 2080.00 250.00 300.08 3508.00 480.0 88 450. 00500.00 1 1 1 f 1 ' 1 i ', i i i i I i : I 1 1 1 : 1 " , I I f.., 1 i 1 1 1 -1-4-1-- 1 1 1 1 1 5 0.0

408.0 + HI--++ hI- -l- -I 1 I---I-- I I-I - I- + + - -- + +-+-I---- -I H ............-.. .. . . + .. .. .. 4-..I-+.. . 408.08400.00 , , , . i i , , , I , , . , , i f f , , , , , , i , , , . , , . ,. , , 400.0,

0 ,-. . . .. . . ', . . . . . . . . . . .. . . . . . . . . . 500 08

i8B.BO . . . . . . . . .- . . . . . . . . . . _ ' . . . . . . . . . . . . . . . ' . . . . . . . . . . . . . ' ' ,_ , : , ; I I . . ...

8

* c CC C0 C

.00000 .8088

.0

.1 350100. i.o i 0.0 200.0 250.00 300.0 353.00 400.08 458.08Aqmtth

Page 109: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SPF CSS-FST RUN 48, 0 DEG SKEW HJT. TIME 258 SEC TIME DAY HR MIN SEC MILL

PLOT NUMBER 12 AZIM VS DEFLX10B.D TEMP-STA 2664 FST. PT.016 13 18 18 857 Figure li.14

s Design c Deflectiontemp.

00eo 50. 000 ±68. B 150. 6 288. 0e 25. 0E 300.00 350. 0 400. 450. 00

480.600.

4"6.088 . . .-..

. ..-4-+++-4-4-4-.

. ._7 .+ .I. . I . . . .. 400.00

2 0 0 '.. . . . . . . . . . -. . .

3 0.* " . i . 6

8 4

. C C. C

SC CC

C.0 6- ... . ..... . . . . . . ...

C C

-r4

,-200.0 41 1 1 .00 45 0.00

eoe0 50. one 10o. 00 ie. 200. e00 250.0 o 300.0 350.00 4N1. Of? 450.03

Page 110: NASA TECH ICAL NASA X-71521 MEMORANDUM · synthetic webbing supported by 6-inch-diameter aluminum pipe frames. The photograph in figure 3 shows the full-jettison catch net in position.

SPF CSS-FST RUN 48, 0 DEG SKEW HJT, TIME 275 SEC TIME DAY HR MIN SEC MILL

PLOT NUMBER 12 AZIM VS DEFLX100,D TEMP-STA 2664 FST. PT.016 13 10 10 857 Fge l1.1

e Design c Deflectiontemp.

. t m000 50. 000 18800. 158.08 200.00 250.00 300.00 350. 00 480.00 4580.8

00.0

-t--4-I ....0- I 680.0010- .0Mo.

c c

0 --

( D 0T5 0 01. .0 0. . .. .- .2. .. ..... ... .. ...... . . 0 0 . 0

16oA035 -60 .13