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NASA TECHNICAL :_:: NASA TM X-53366MEMORANDUM 4
j.. December 8, 1965 -_--T
L- X
N66-1_+782 ::_
- j¢0 -, '_ ¢CODID
:'_. I_ - (CA'rKGORY) "I _ GR OR _ OR AD NUMblY.R)
_" " I_.. r_
- Z
_- VIBRATIONANDACOUSTICANALYSES_ SATURNSA-IOFLIGHT
_'-_ by MEASURING AND EVALUATION SECTION" Propulsion and Vehicle Engineering Laboratory
:_.
I,=- GPC- Pi';CE $
: CFST! Pii|CE($) $
Hard copy (HC), i
GeorgeC_Nat&all ..._o,,_oSpace Fl,ght Center,
Huntsville, Alabama /
1966005493
https://ntrs.nasa.gov/search.jsp?R=19660005493 2020-01-07T03:53:43+00:00Z
TECHNICAL MEMORANDUM X-53366
_XBRATION AND ACOUSTIC ANALYSES
SATURN SA-10 FLIGHT
' By
Measuring and _valuation Section
George C. Marshall Space Flight Center
Huntsville, Alabama
ABSTRACT
This report presents an analysis of the vibration _nd acoustic
. data measured during the fligh_of SA-IO. Instrumentation and equip-
ment used in the data acquisition and data reduction systems aredescribed. The effects of the vibration and acoustic environment on
the Saturn S-I stage, Instrument Unit, and Pegasus structure are
* evaluated. Structural response is described and presented pictorially
in terms of power spectral density versus frequency. Internal Saturn
SA-IO acoustic environments are discussed in terms of sound pressure
spectrum level versus frequency. Installation sketches of all vibration
and acoustic transducers used on the SA-10 flightvehicle are shown.
NASA-GEORGE C. MARSHALL SPACE FLIGHT CENTER W'
.,' .bL/
1966005493-002
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1966005493-003
NASA-GEORGE C. MARSHALL SPACE FLIGHT CENTER
TECHNICAL MEMORANDUM X-53366
VIBRATION AND ACOUSTIC ANALYSES
SATURN SA-10 FLIGHT
By
Measuring and Evaluation Section
.j-
._-,"_.._
° . _
• ":f
•, VIBRATION AND ACOUSTICS BRANCHS TRU C TU.RES DIVISION
PROPULSION AND VEHICLE ENGINEERING LABORATORY"C
RESEARCH AND DEVELOPMENT OPERATIONS . ,1'
5,
1966005493-004
!
i
• =
ACKNO W LE DGEMEN T
This report was prepared by Chrysler Corporation
Space Division, Huntsville Operations, Structures Branch
, of the Structures and Mechanics Engineering Department..
for the George C. Marshall Space Flight Center, Propul-
sion and Vehicle Engineering Laboratory, Structures
Division, Vibration and Acoustics Branch, under Contract _ _• i
NAS8-4016, Mod. 80, Task D.
}
Iii • f.-
.. i_!
/
1966005493-005
#
TABLE OF CONTENTS
Page
I. INTRODUCTION .................... 1
II. DATA ACQUISITION . .................. Z
HI. DATA REDUCTION .................. 3I
IV. VIBRATION EN%q..RONMENT ............ 5
A. S-I Stage Structure ................ 51. Shear Beam/Shear Panels ........... 6
Z. Spider Beam/Upper Structure ......... 7
B. S-I Engine Components .............. 71. Thrust Chamber Dome ............ 72. Turbine Gear Box ............... 8
C. S-I Fuel Tank Skirt Component .......... 84
D. Instrument Unit .................. 9
I. Guidance System ............... 9
# Z. Structure ....... ............ 103. Components .................. i0
E. Pegasus (Apollo) ........... iI - "-"":t,
"-:
F. Special Low Frequency Instrumentation (Pegasus) 11 2:_:
- t_:,
V. ACOUSTIC ENVIRONMENT .............. lZ .- _
._. S-I Stage ...................... IZ "x'
B. Instrument Unit .............. 13 , :_eg_o , • • • . °,-
" C. Apollo Adapter ................... 13 _ : ":"?'_"
.. - ._:._
'._ " _.. _" "_"-,_,::_-,_.
] 966005493-006
L;._o
t
TABLE OF CONTENTS (Continued)
Page
APPENDIX °
i A. Measurement Locations .......... . . 14B. Vibration and Acoustic Data .......... 3Z- *
p
0
_t
iV
1966005493-007
#
!
LIST OF ILLUSTRATIONS
VIBR ATION ENVIRONMENT
" S-I STAGE
Meas. Meas. Meas. Loc, Reduced Data
No. Description Page No. Pa_e No_f
EII-Z Thrust Chamber Dome 15 N/A*
Eli-4 Thrust Chamber Dome 15 N/¢I ._
Eli-6 Thrust Chamber Dome 15 N/A5
Eli-8 Thrust Chamber Domc 15 N/A ;: --
EIZ-I Turbine Gear Box 15 33 _
EIZ-Z Turbine Gear Box 15 34 _
E12-3 Turbine Gear Box i5 35 :_?
E12-4 Turbine Gear Box 15 36 _ ,,
EIZ-5 Turbine Gear Box 15 37 _ :,'_:'_:-
E12-6 Turbine Gear Box 15 38 _"" ... .-_",_,':
EIZ-7 Turbine Gear Box 15 39 '-*---_;._:
E12-8 Turbine Gear Box 15 40 - "-"_;:_"
E33-I Th, _,$_Chamber Dome 15 N/A : ".:<_
E33-3 Thrust Chamber Dome 15 N/A :......
E33-9 Thrust Chamber Dome 15 N/A i:_:._..:'_
,, E33-7 Thrust Ch ambe r Dome 15 N/A ,,.... .k:'.._,-_':5_i__.:_..
*Not Analyzed -."__,..$_
.-_:.._"._?
1966005493-008
tf
ii
•I LIST OF ILLUSTRATIONS (Cont;.nued)t!
I Meas. Meas. Meas. Loc. Reduced DatalNo. Description Page No. Page No.
I
E105-U Spider Beam, Long't 16 41
i -. El07-11 Spider Bea. m, Yaw 16 42
: _ E135-9" Shear Beam i7 43
_.- .i E136-9 Shear Panel " 17 44i-
_i! EI39-9 Shear Panel 19 45
!iiiiill E140-9 Shear Panel 19 4-6E270-9 Distributor ?A3 Mtg. Brkt. 20 47
;!t TNS'I RUMENT UNq@'--11 Eg0-80Z Inertial Gimb_] ST-124 21 48
E91-802 Inert{al Gimbal CT-i24 21 49f
E9/.-802 Inertial Gimbal S'r-lZ4 7_) 50
E93-802 Mounting Frame ST-IZ4 :_: = 51
E94-802 Mounting Frame ST-124 Z_. 52
E95-802 Mounting Frame ST-124 ZI 53
_ E345-802 Support, ST-124 22 54
E346-802. Support, ST.-I24 Z2 55
ii " " ' "E347-802 Support., ST-124 Z3 56 "*'::"
E348:802 Air Bearing Supply 24 57
• ;.. |'" . - . ;
.. \
- _
J
, ,-. , .,.' ) : - .
1966005493-009
I
• ..._
LIST OF ILLUSTRATIONS (Continaed)
M_as. Meas. Meas. Loc. Reduced Data
No. Description , . Pa_e No:, Pa_e No. "
E349-80Z Air Bearing Supply Z4 58 "
E352-80Z RF .Assembly 25 59 ---I _ " ._:.
E353-80Z RF A.ssembl 7 25 60 _ . .. ::._-.
E354-$02 Guidance Computer Suppo1"t Z6 61 . "-"--:_"_":_:'"_-. -Y'-:.---"-":-__i
E355-802 Guidance Compute-- Support Z6 62 i -: f_ _i_i
E356-SOZ Guidance Computer Support Z6 63 _ " " _:_!i!_" ..--_.- ,-_-,_.
E359-80Z Upper Mounting Ring Z5 64
l
_-..- ..:. :_.:E360-80Z Upper Mounting Rin.g Z5 65 .......... :_,:.
E361-802 Lower Mounting Ring 25 66 " " _L_'_
_._ :._< _°,.-._._"t E362-802 Lower Mounting Ring 25 67 _:.-.;_:¢_
_._-.-. _,-._
E379-802 Upper Mounting Ring Z7 68 !;_._;_._ -_
E380-802 ._per Mounting Ring Z7 69: !_-:
_," -'': _._
E381-80Z Lower Mounting Ring Z7 70 -"- "-'-,;__., ':;. _._._:
[E38Z-80Z Lower Mounting Ring Z7 71 . "L:_.-_,,:_-,_,.
E369-900 Upper MMC Mounting 28 72 :_'_.._;,_.
E370-900 Upper MMC Mounting 28 73 - _
E371-900 Lower MMC Mounting " 29 .. 74 :_" .
E372-900 Lower MMC Mounting Z9 75 _'_
... " . - ,.
1966005493-010
5-r.-
_': LIST OF ILLUSTRATIONS (Continued)i-
: Meas. Meas. Meas. Loc. Reduced Data
_. No:.._ Description ,l_.age NO. .P,.z.ge No.
_.-E375-900 Upper MMC Mounting 30 76
i Longeron No. 3
: E376-900 Upper MMC Me,rating 30 77
Longeron No. 3
_-_384-900 Top Tie Point MMC 31 78|
ACOUSTIC ENVIRONMENT| :j
S-I STAGE
L28-9 Internal Sta. 172 18 N/A
TNSTRUMENT UNIT "
l L66-802 Internal Sta. 1480 Z2 79PEGASUS
L70-900 Internal Sta. 1495 29 80
!
[i: viii
1966005493-011
LIST OF S_ MBOLS
B.W. bandwidth
cps cycles per second
dB decibel (reference 0.0000Z Newton/meter Z)
ES'r eastern standard time
F-1 fuel tank no. 1
F-2 fuel tank no. 2
G dimens ionles s accele ration value
G 2 mean square acceleration value
GOX gaseous oxygen
IECO inboard engine cutoff
I. lJ. instrument unit#
Mach I speed of sound in air
max Q period of maximum dynamic pressure
I
OECO outboal -1 engine cutoff I.:
PSD power spec::ral density (GZ/cps) J "_"
RF radio frequency " _-
RMS, rms root-mean-square _'_!• ._ _ _ ', _.'
-" _ -_.'=.._oS-I Saturn first stage i .-'. '"'"
S-IV Saturv second stage _, ".._.:_'"1 ; ." ,._
sec seconds
,'.-. .. - -¢:.%_:.• -.';.,_ o: .
•,_ . ._,,..."' _,_
• _., A-':._'_"
] 966005493-0 ] 2
BLANK PAGE
- . o .
._. . ..... ,. , .. -
" - U
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1966005493-013
TECHNICAL MEMORANDUM X-53366
VIBRATION AND ACOUSTIC _ NA LYSES
SATURN SA-10 FLIGHT
SUMMARY
l
The SA-i0 vibration and acousLic environments were normal
and did not exceed expected levels. In general, the S-I stagevibration environments compared closely with previous Saturn I,
Block II vehicles, l'he high vibration levels measured on the shear
panel measurements on SA-8 and SA-9 were ._o= present on this
flight.
The SA-!0 vehicle was the third to fly a prototype model of
the production instrument unit (I. U. ). The vibration environment
recorded on this flight ag=eed closely with the past history envelope
established on the flights of SA-8 and SA-9. V{bration of the I. U.during S-IV powered flight was negligible.
The Pegasus satellite data exhibited good agreement with the
past history envelope established on the previous two flights.
Vibration during S-IV powered flight was extremely low, Internal
acoust';c _uvironments of the instrument unit and the _pollo adapter
showed an excellent comparison with past history levels and with the
predicted time history. The acoustic data obtained from the S-I stage .':was not reliable.
.- _'--,._;
; I. INTRODUCTION ._%_
The Saturn SA-10 vehicle was launched at 8:00 a.m. EST on:%
July 30, 1965. This vehicle was the final Saturn I configuration to be _flown. The SA-IO vehicle comprised the S-I stage, S-IV stage, -_._--.
instrument unit, a boilerplv=e model of the Apollo spacecraft, and ' " "=-_
the Pegasus satellite. ': '-_.
•, A discussion of the instrumentation and data acquisition :_• -.,,_.
systems is presented in Section II of this report. Information is _-_-:_-_
given on the distribution of vibration and acoustic measurements by . _
vehicle stage. The operating characteristics of the data acquisition . ----._and
signal conditioning equipment are described in functional sequence. ; " _",_-,-
._ - ":._.j._
q966005493-0 q4
The data reduction system and related equipment are de- i
scribed it, Section HI. A discussion of the role of the digitalcomputer in the reduction of all measured data is presented. In
addition, a flo_- chart is included to show _he complete data acqui-
sition and data reductic-n process, o
An evaluation of the vibration environment is presented inSection IV. Emphasis is pl_ced on the abnormal structural response
I ¢h&racteristics. A discussion of the significant aspects of the lmeasured data is given for each grouping of component or structural
measurements.
The acoustic environment is evaluated and discussed in
Sectt&n*V. This evaluation shows the signifY.cant aspects of the
internal acoustic environment during launr_h and of the aerodynamic
environment induced during the region cf maximum dynamic pressure
(max Q).|
The appendices include ins_.allation dra_-:.ngs __or the vibration
and acoustic transducers and present the reduced data in terms ofGZ/cps amplitude versus frequency and amplitude versus ti._u_-. _,
IL DATA ACQUISITION$ i
The SA-IO vehicle was instrumented with 54_ vibration trans- 'J
ducers and 3 acoustic transducers, clistributed as foUows:
Vibration Acoustic Total
S-I stage ?-3 I 24Instrument unit 24 I 25
ApoUo
High frequency 4 I 5
Low frequency 3 3 _.s"T- -T-- • !• • ]
The data acquisition system for the vibration and acoustic ]data consists basically of a transducer, emitter Iollower, amplifier, I¥
multiplexer, transmitter, receiver, demultiplexer, and recorder. _
Z
i
1966005493-015
o.
The SS/FM telemetry systems utilizes frequency division
multiplexing techniques to transmit the multiple data channels on a
common RF carrier. The analog voltage from each transducer
amplitude modulates a 455 kc channel carrier signal. The output at
• the first modulator, with the lower sideband removed by filtering, is
transposed upward in frequency by a second modulator to its assigned
position in the multiplexed spectrum.
The multiplexed signals are transmitted from the vehicle over
ultra-high-frequency (UHF) radio channel and are detected by ground
receiving stations. The receiving portion of the single sideband
system reverses the process of the transmitting portion. The receiver
output is fed through a demultiplexer and each channel is transposed
from its assigned position in the spectrum to its original frequency.
IH. DATA REDUCTION
At MSFC, the magnetic tapes are demultiplexed and the• vibration and acoustic data is re-recorded on individual data channels.
In this form, the data.may be analyzed with the random vibration
analysis program (RAVAN). This program was developed by the
MSFC Computation Laboratory for use in conjunction with the IBM
• 7094 digitalcomputer. A flow diagram of the complete data acquisi-
tion and data redaction processes is shown [n Table I.
The RAVAN program performs an analysis on the random _' i
vibration data by computing the firs_ four statistical moments. Thesemoments are the mean value, standard deviation, skewness, and
o'_
kurtosis. :-_ -_
The most useful data obtained from the program are in the -i_"__spectral analysis format. Spect.'-aldensity plots are employed to -'_
define the frequencies of mos _. severe vibration and the energy content _ -.-:_
of portions of the spectrum, it is important to note that the power _-:_"
• spectrum is the Fourier transform of the autocorrelation function. _ ''__
The vibration power spectrum, in terms of mean square ._ _:_:
amplitude per cycle per second (GZ/cps), and the sound pressure _ " --::_" spectrum level, in terms of decibels per cycle per second (dB/cps), _ :'-_._._
are the most convenient spectral analyses for engineering applications _ _ :__:_'
. . ¢
and are the ones presented in this report. • __
1966005493-016
%
The spectral plots presented in Appendb_ B show the maximum
response amplitudes (GZ/cps or dP/cps) that occurred during powered
flight. In general, these maxima occurred during launch and max Q.The launch spectral analyses were not available for all measurements°
of time-shared telemetry assignments. For the._e measurements, the •
maximum available spectra are shown for t_e indicated fiSght times.
"I_ne vibration and acoustic data were analyzed with an effectivebandwidth of ten cycles per second. No correction factor has been
added to _he data to account for the roll-off in the te!emetry system
frequency response. Therefore,_ribration and acoustic amplitudes
below a frequency of Z00 cps have been attenuated (from 0.5 dB at
Z00 cps to 4 dB at 50 cps). Data amplitudes below 50 cps should be
disi'egarded.
: TABLE I. Telemetered Data Acquisition andData Reduction Chart
Jl Transducer HSigna2 Conditioning HI Tran_tter t
I .....
I ,,,.o,.1.---4,,,,,,.n,,,,,,',,,,,,,. t"4 ,,.,,,0,,,v,,,. I,I,!
,t,• -'._
: Zonal Statistics Reformat Meas. Var_auce '
• ¥
¢.fJ_-:I"'
%_:°"_
1966005493-017
IV. VIBRATION ENVIRC, NMENTS
The sources of vibratory excitation.for the Saturn vehicle may
. be classed in three catcgorics:
i. Acoustic
Z. Mechanical
3. Aerodynamic
The acoustic noise is generated by the turbulent mixing of the
engine exhaust gases with the surrounding atmosphere. It is most
predominant at launch and gradually diminishes as the vehicle velocity
approaches the speed of sound. Acoustic noise is the most damaging
to skin and panel structures and to electronic components.
The mechanical vibrations are generated within the enginecombustion chambers and take the form of structural vibration. This
vibration is transmitted from the engines through the thrust structure
and up into the vehicle. The mechanical vibration is most damaging
, to structures and components located adjacent to the engines. ' :
The aerodynamic source is generated by the turbulent boundary
layer surrounding the vehicles as the speed approaches Mach 1 and
t the vehicle passes through the condition of maximum dynamic pressure
(max Q). These sources are often compared to the acoustic source -
because the pressure fluctuation effects are similar. Aerodynamic ":,_
excitation is unost damaging to the exterio.r structures and components ."_'-attached thereon.
The vibration environments measured during the flightof S_-I0 '",_.. _ .;_:'"
.compared favorably with the Past history levels established on pre-vious Saturn I, Block 11 vehicles. The maximum environments for _!_
the S-I stage and the instrument unit occurred during the periods of :, -,
launch and maximum dynamic pressure. Vibration excitation was ,..,-'-_
extremely low during the S-IV portion of the flight. No evidence of -,. .,/_,_• structural fatigue or component malfunction was noted during the , -
flight. '-,. . . -,-.y_.
A. S-I Stage Structure _. :,.. ,,.:_;
The SA-10 S-_ stage structural vibration was measured _ " _
with seven accelerometers. All telemetered data were valid,throughout i_. ....." -,_i_):__
i.F{_p_..--,
1966005493-0] 8
i powered flight. The measured response of the S-I stage structure
was normal and did not exceed expected levels.
Maximum vib,'ationwas induced by the acoustkc and aero-
dynamic noise environments present durin Z launch and max O. °
j :I. Shear Beam/Shear Panels: (E135-9, E136-9,
• E139-9 and E140-9_
The thrust frame structure was instrumented in
three locations with four accelerometers. Transducers were located
on the shear panel and the "E" beam between fin lines III and IV and
on the shear panel between fin lines I and II. The shear panel trans-
ducers were located adjacent to the attachment of the shear panel andthe respective thrust post of engines No. 1 and No. 3.
The composite response amplitude of the shear beam measure-
ment (E135-9) showed excellent correlation with the past history
envelope. A maximum ainplitude of 7.03 Grms was recorded shortly
after max Q. The SA-8 maximum was 7. 5 Grms during the same
flight period. The predominant frequency noted during critical flight •periods was 600 cps. This compared favorably with the 570 cps•recorded on SA-8.
The composite response amplitude of the shear panels betweenfin lines I and II was similar to that obtained during previous Saturn I,
Block H flights. Greatest excitation Occurred during the launch,Mach 1, and max Q periods of flight. A maximum vibration level of
13.71 Grms was recorded during launch _ the axis perpendicular to
tlte panel (El40-?). This amplitude was 2.81 Grms higher than thatrecorded on SA-8 during the launch period.
The composite response amplitude of the shear panel located
between fin lines IH and IV (E136-9) appeared to be normal throughout
• flight. Tl_e response on SA-10 was 12.2 Grr_e less than SA-8 at
T + 90 seconds. The data obtained on SA-I0 compared closely withthat received on SA-5 and SA-6.
An effort is being made to correlate data from E136-9 on
flightsSA-9, SA-8, and SA-10 to engine No. 3 performance. "£his
. _rreg.ular re'sponse phenomenon note d on the past three flights seems
1966005493-019
to be related to the chamber pressure of engine No, 3. However, thedata from the combustion chamber domes Ls again questionable on
this flight. For this reason, vibratory excitation from the engines
cannot be adequateIy defined or correlated with shear panel response,w
2. Spider-Beam/Upper Structure: (El05-11, El07-11) ...
Spider beam response to vibratory e:ccLtation was
measured in two mutually perpendicular axes, Acceterometers were
located on a radial beam of the spider beam structure along fin line I,
The response at the exterior location (spider beam) was genera]l 7
consistent with previous data.
As expected, vLbratLon at the exterior spider beam spoke Was
greatest in the yaw-axis (E107-il). A maximum composite response
of 9.94 Grm s (predominant at 590 cps) was measure_d {n this axisduring max Q. Thi's compared with a maximum SA-8 composite
response of 7.54 Grin s at the same flLght event, The SA-8 excitationwas greatest at 590 cps.
* A maximum composite response of 5.57 Grin s was measured : .
_n the longLtudLnaI axis (El05-11) at holddown " The predominant
frequency was 1404 cps.. _-
¢ B, S-I__Engine Components _, ._".:.".,
Sixteen vibration measurements were made on the S-I _ " :""--__._.•:-_
stage engLne components. These components included the combustion -_: . .: _'
chamber dome and turbLne gear box. The vibration envLronment • _ ,.-_-._.-_. :_
not,. d ov the turbine gear box measurements _ndLcated a normal S-I ' . ._-,:=-• . _.i_ _
powered flight. The data obtained from _he combustion chamber dome i._:_:_.measurements were not considered valid, :.... _°
1. Thrust Chamber Dome: (Ell's, E33's) ;
. _ : . -._..... _._,.The v[bratLou of the thrust chamber domes was. . _.:.:,.,,._._-
" measured in the lateral d_rection on engLnes No. 2, 4, 6, and 8 and - !"'s-__:_:__!__:_in the long_tudinaI direction on engines No. 1, 3, 5, and 7. w:.._:..._..?_
I:::._'_{"-._._"The vibration envLronment of the thrust chamber domes has ' '.-.--._.:_.-_,-
. .- .%.._-_.
not been defined satisfactorily on any Block H vehicle, It has been .... _:--;'_:-
• . . .___'_
_._:_,:-:7 """-"_..':
:...._.-
1966005493-020
\
concluded that telemetry instrumentation from this region is affected
by some type of external environment that prohib[ts the acquLsLtLon of
valid vibration dat_• Further studies are beLng performed to define
this problem.
Z. Turbine Gear Box: (EI2-1 through E12-8)
The SA-10 vehicle was the first to employ a gear
box measurement on each of the eight booster engines. Each acceler-
ometer ir, ea_ared vLbratLon in a direction parallel to the pump axis.
i 'the vLbratory responses showed excellent agreement with th_ levelsi establ_shed on previous Block H vehicles.
""
j The predomLnant response frequencies assocLated with the
turbopumps were approximately 1100, 1600, and 2200 cps. TheseI frequencies shLfted upward by about 50 cps during powered flLght
i LndicatLng an increasing turbopump rprn as flight progressed.!
• ! "The eight turbine gear box measurements showed a constant_' .|
co'_'_ osite response throughout fEght wili_ a maximum of 36 Grin s"_" " ,'i
_i rP" orded on E12-4 just prior to t/_e engine cutoff sequence at_'_:i. T + 142 seconds. The highest discrete frequency arnplitude during:'_ this period was 5 Grins at 2200 cps.
• C, S-I Fuel Tank. SkLrt Component •
There was one accelerometer attached to the ring fralae
Ln the lower skirt region of fuel tank No. 1, adjacent to the 91%3
_ dtetrLbutor. The response amplLtudes and frequencies were consistent
with the response parameters measured during prevLous Saturn I,Block H flights.
Vibratory response of the ring frame in the lower skLrt reg{oni!._ of fuel tank No. 1 was measured near the point of attachment of the
9A3 measurLng distributor mounting bracket (E270-9). Data from a
IongLtudLnal sxLs vibration measurement at this location are indicative
!_ of {nput excLtatlon to the distrLbutor mounting bracket. *
9 The maximum composRe response reached 3.9! Grin s nea,max Q_ The predominant frequency associated with this amplitude
• was 95 cps. The corresP0nding SA-8 maximum was 3.54 Grin s at425 cps,
6. :-.- -. J -
1966005493-021
!
D. Instrument Unit
The instrument unit vibration environment was monitor-
ed with Z4 accelerometers. The structural configuration was thesame as that of SA-8 and SA-9, The I.U. vibration levels of S.A-10
showed good correlation with those obtained on SA-8. All Z4 measure-
ments gave good data throughout powered flight.
I. Guidance System: (E90-802 thi-ough E95-802, •
E345-802, E346-802, E347-802)
The vibration environment for the .._'" 124 guidance .
: system was Very similar to the levels, recorded on the SA-8 and SA_9
vehicles. The response levels were minimal except during the.Mach
1 and max-O periods of flight. ,i--.
The vibration levels between the mounting frame and the _.--.
inertial gimbal were attenuated to a lesser degree than they were .:
during the SA-8 flight. The attenuation between the support structvre ._:"_--.-_
and the mounting frame was much less than on the SA-8 flight;how- ...,-.:_,_
ever, the attenuation corresponded well with the SA-9 flight, .::_
The vibration of the ST-124 guidance system was measured '-:"
on ,he inertial gimbal, the mounting frame,'and on the support' .:_
t structure. The support measurements were located on the upper ""._ _mounting ring near the point of attachment of the mounting frame: and : . : ..,..":'_*_"*,_.
the upper mounting ring, ..- ,. _"_"
The inertial gimbal measurements (E90-802 through E92-802), -' ' _- " _ ?_-
mounting frame moasurements (E93-802 throug_ E95-802), and the _'-"_',*-_-,_._.:._..
support measurements (E345-892 through E34_-802) all recorded ._.._-._.._
vibration levels that agreed with the past history environment • :_..--_ _:__,
established on SA-8 and SA-9. _5.'_:4_":-_.-_i-_-'..•_._
The maximum respf::._se recorded on the inertial glmbal was :. _.._._
0.4 Grin s at 180 cpe in the pitch direction at max (2 and 0, 4 Grin s at ..... ,i.-
lZ0 cps in the pitch direction during liftoff. ._:':._--_-_-_
The mounting frame response showed the highest amplitude, ,._:.:j_._-
1.4 Grin s at 175 cps recorded tn the longitudinal direction at liftoff. _--_,._r'_._ _:
_.,-.:.._..,_,
1966005493-022
t
_ The maximur_ response on the support structure was 1.2
Grins at 1534 cps at max Q.
: g. Structure: (E359-802 through E36Z .8OZ,
,_ E379-80Z through E382-80Z) •
; The I.U. structural vibration environment was
-" measured by eight accelerometers located on the upper (Apollo) and
lower mounting rings. The 3A-10 transducer locations and structural "
configuration were identical to those of SA-8 and SA-9.
-; A comparison of SA-lU flightdata with those of SA-8 and
; SA-9 revealed that the SA-I0 composite vibratic.n levels compared
favorably with the past history envelope est_.blished by the two, previous flights. The maximum composite level recorded for SA-10 i
, was 7.9 Grm s occurring at liftoff. This level was recorded bymeasurement E382-80Z, located on the lower moun::ng rings between
fin line IH and IV perpendicular to the flight path.
i The maximum response of the lower mounting ring of the I U '
structure was 1.46 Grms at 505 cps. The upper (Apollo) mountingring experienced a maximum response of 0.74 Grins at 695 cps. i
i
Vibration levels measured on hhe I.U. structure during S-IV i,
powered flight were minimal. ' ig
3. Components: (E348-302, E349-80Z, E352-802through E356-80Z)
I The vibration input to various components within
the I.U. was measured on the honeycomb panel support structure
with seven accelerometer, s. The composite vibration amplitudescompared very closely _viththe SA-8 and SA-9 levels and were not
considered to be detrimental to the proper functioning of the air
supply, RF assembly, or the guidance computer. As had been
observed during SA-8 and SA-9, the vibration perpendicular to the f
i panel surface was the highest for all three measurement groups, * i
|The air bearing supply (E348-80Z and E349-802) experienced I
a maximum input of 1.7 Grins at 235 cps during liftoff and 1 Grr_.3 at _ I245 cps at max Q.
i::t']b
10 :
1966005493-023
The input to the RF a_sembly (E352-80Z and E35B-802) reach-
ed a maximum of 0.7 Grins at 155 cps during liftoff and 0.5 Grin s at
t55 cps at max Q.
• The input to the guidance computer (E354-802 through
E356-802) reached a maximum of 0.7 Grms at 220 cps during launch
and 1.3 Grms at 220 cps at max O.
" E. Pegasus (Apollo) Vibration: (E369-900 through E372-900)
The vibration environment of the Pegasus micrometeo-
roid capsule (MMC) was measured by four accelerometers located-on
the mounting structure. Two measurements were made at the upper
end of longeron No. 6, adjacent to the point of attachment to the
Pegasus, and two were made at the lower end near the point of
attachment to the A. pollo boilerplate structure. The vibration levelsof SA-10 compared closely with the past history envelope established
by SA-8 and SA-9.
The maximum response at the upper point of attachment, (]_369-900 and E370-900) was 0.65 Grms at 495 cps during launch,
and 0.61 Grins at 395 cps at max Q. At the lower attachment point(E371-900 and E372-900), the maximum response was 0.47 Grms at
580 cps during launch and 0.36 Grms at 260 cps at max Q.
The vibration levels recorded during S-IV powered flight were
considered negligible.
F. Special Low Frequency Instrumentation (Pegasus): -_
(E375-900, E376-900, and E384-900)
Three tow frequency vibration measurements were ._.A._installed on the Pegasus MMC to survey vibration environment in --
the 0 to 35 cps range. E375-900 and E376-900 were mounted on _ "_._--
longeron No, 3 at approximate otation 1580. E384-900 was located -_ _-'_
at the top tie point hub assembly, statio_ 1768.5. E384-900 and _, _7:_..
-- ._- _i_._"E376-900 measured vibration in the lateral direction, or perpen-
dicular to the line of flight. E375-900 measured the vibration in the ._ . -._
!ongitudinal direction. Measurements E375-900 and E384-900 : .
showed a close correlation with the low frequency data obtained on _ :'-" ,qA-9. .,
.4 ._ _."_.
_,.-
1966005493-024
The maximum response denoted by _375-900 was 0.09 Grins
at 11 cps at liftoff. E384-900 indicated a maximum response of
0. 056 Grin s at 7 cps, also at liftoff.
Measurement E376-900 showed a marked increase in
vibration environment over the SA-9 flight data. A composite level
of 3.36 Grin s was recorded on SA-10 at liftoff compared with 0. Z6
Grin s on SA-9 during the same flight event.
The maximum response of E376-900 was 0.58 Grin s at 6 cpsat liftoff compared with 0. 075 Grm s at 15 cps on SA-9, also at liftoff.
Since low frequency data have been reduced on only SA-9
previously, it is difficult to establish w,hat a normal response forthese measurements should be. In addition, the fact that E384-900
" showed very low vibration levels in the lateral direction leaves some
question as to the validity of the high levels recorded on E376-900.
V. ACOUSTIC ENVIRONMENT
Three internal acoustic measurements were made on the
SA-10 flight vehicle. One measurement was located on the U'rust
' structure of the S-I stage at station 171.75. The second x._easure-ment was located in the I.U. at station 1480, and the third was
located in the Apollo stage at station 1495. The measurements on
the Apollo and I.U. were in good agreement with the predicted levels
and the past history environment of SA-8. The S-I stage acousticmeasurement was considered invalid.
A. S-I Sta_e: (L28-9)
The acoustic measurement on the S-I stage was made atstation 171.25, 2Z. 5 ° off fin line III toward fin line H in the thrust
|
structure area. This measurement was inv_lid._nd no usable data; were obtained. The character of the data indicates that it is possible_] that condensation from the thrust area caused a malfunction in the *,
" " I data acquisition system.!
-ii w
-!I
."!
_'_-." .
"___• _,
196600549g-025
B, Instrument Unit: (L66-802)
The internal measurement on.the I.U. was located at
station 1480, 45 ° off fin line II toward fin line III. The acoustic
* environment agreed very we!l with _he predicted and the measuredenvironments established on SA-3 and SA-9. The most severe
acoustic environment measured during launch was 138.5 dB; atmax Q, IZ8.5 dB.
&
C. Apollo Adapter: (L70-900)
The internal measurement in the Apollo adapter was
located along fin line I at station 1495. The highest environment
was 139.5 dB measured during launch. The in-flight environment
near Mach I and max Qwas 139.6 dB, 5 dB higher than thatmeasured during SA-?. The SA-8 environment was comparable to
the SAo 10 environment during the period of Mach I, however the
max Q levels were more comparable to those during the flight of SA-9.
The change in the acoustic environment at this location is the result
of the addition of a control motor along fin line I upstream of this• measurement location for flights $A-8 and SAoI0. The motor was
mounted externally and protruded into the boundary layer flow
.generating shocks and turbulence that influenced the acoustic environ-
ment immediately-downstream. In contrast with SA-8, this excitation
• persisted in the SA-10 flight through max Q because the positive pitch :-.
angle created a thicker boundary layer than was generated in SA-8.
F
... -,,-
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1966005493-026
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BLANK PAGE
" _7"#
1966005493-027
APPEND_ A
ME_AS UR EMENT LOCATIONS
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1966005493-031
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1966005493-032
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1966005493-038
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1966005493-042
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1966005493-044
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1966005493-045
I
i
Meas. No. _.!2-I
• "+....... ....... - G.=Box4.1".,i,..L.:it|l:l|i..'|| |i|,.ti,;t.|,_ """ I"::': -...w . ... : ,.| , t:s.L._i,..1::.I_':'.......;._., . ,:..,;,L.I.:,.._..... ,,....:-,:,-,':I"
.I ;. l.il.i-',.i |.., f if, :,II: lll;-|;_'ii'|'{ 'ii"'ii':"i'i "|'| is'|'l|i'l''={i'|"
• . .l.s l|='i|..lli.,.,l,|i'..|. . I.|= ,-ii,'l ,:;'|.=,.;.p., i|,.|;;|;l.-.i..t'|" --I • ' . _ l'l L ..LS,.I.L_s -S
• ="if' I ,:"i "l"li'&i|j'li'f'i|||Lll'T" " • "'l" "|" ;' ;,"1" • T........ ;., ,, , , . ,.h.'..' ..... i,. ,,,..,i ..... Sensitivity Parallel %o Pump Axis
..., ,.:I.,..,,,I..i.ID.;|,I|,|_..L_..I..;|; ! lhi.. !,...i, ......i,.. ;'!.'_'.",_"
•o.,.t,l*i.|s_,||T,_t.|t- ."4_,.t1|'|_ _"
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I -:..li....,,,_,i,,,i,4_,...:i,!i.,,,-'_ _ ,i,i":'#-'",; .'!,_:,t._:l"._..... _ Remarks• i|_ l.,_.,||1.s_%i|i_.tl=ili,._.;,||t._|_l &t&tl-t'tltsit.= "q;1_"; IILs. ;H%- ---_= ""
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"l/" b" I/ 'h" 'l/ "I/ '-'" "J '_"'-'J " " "' '_ "
Tn4_E H_STORY ' _=
Meas. No. E12-2
........ •. ,,...... :;:.;.......'_.-!:";.;;";" ";;:: . -"'. "'".:......;|..,..'...._,:,..,I,.....,...." ...... ..., . .., .., • _b_e Box......................... ;..... ::.:..i ....................... - -- wescr,p_,on
• , ........ ,.,.'...Iol...I.,.-,.:....;,.: ..., ...... : ...... "." ....... ]
° "',':,=', "- ........ ."........ _" ,i.... ", ' , ,,i • En_¢• .r ....... ||,|-lli ........ w,.,,i ........ l_;';;:';;;, :'"_''; |:';;; ..... .............. IIIIlll' "llll I'I I1", ..',.|.1 .... : : ; ...I.. |. .
'.',l:I'|,., =I=IlI, I w|" ' . '= I. =' =.1 I,,, I = . =J == •1 = = .===i = •,
•.,.., " 1.; .I .... =.;,, -" .. • ..,:., ;. ,_.., ,..; , .i,... ..... ..... ....... ,", ................. ' ...... -"i ..... _en-.... _-I to _Psra_el Axis
.,.I .. ;....;. ,,..',, ,.;, :1 . -.: • :: .... :'' =""''W";'" ." "" ....,-..'- ..... "s"m=w==.'* ..'|-'''S,,.'.m'':LS...'.-.:;-.h-=I.| LD..-_..=,.b...tq|...... .. ...I... , .:._ ..,...,.., '... • ,;..'Io.. b|. -'. , .A... ,.....
• .. , . ;I.., .., _j,...: ..11, .-" i _..;. , . , | & l
.... :............... '':'"'"'"':::':'" ........ ". "' '" ..... 'I':" " Location: Page 15" It,,..i,i-..'.:*.T-,,-'-...._. ,,o,:..;'=-.l=.-._..,. .... ._,.I .,.-s- -| ..,-
._ ...... .|. i • .. i ..'l,t ..... 1..I ; i '.. i .... i, , ,. .. • .
.......... : .-,-.,,b .... -,,'- ........ ;....... ,.....-.;,,..-.; ..... I,.,-. Calibration + .50 G• ' "" ".':" "" ". .' , .,|.*...l.:--.- :'.., , ....... ' "'" | ""I":'"
• ., .., |i,.i.,i,, i.i-i .lie. I|. ,,.,:=. : .: ., . ,. i=.'|I .i |I
......... ,..' ,,,..'.a.,....,.,. ......... .'--.."I -' .,:. ,.'..-, ........ *.,., Remarks
.... ;,.,.i'.l.l,'-,[l, :=_-.:.i.--.::.. i.:...',,',,. • -_'. ".;'-:.='--s, : "t• ,._i=i/I,IsS--,i,ii "_. _&_-===="-= ,.,,l ..4_'-_iliIi=,,Is,- :'i. i._. h =.l=.i=,' , • • , , I • I
• ..|..|l_.._li......m_.w....|_.t,...|....|;.|==i | • "=m_,,.,.= = ...... |.,m= |,_,,= _i
• ,; -|,,,n,m ...n,s..s.,, .... m:.hl |,,.s,,:nll..; "|'"n""" • I ..... ;
i t|,'," .,,,,. | -,a_,._,l=_,i'. ,,,i=.,|, ".=_t| ,; • I,_,,=I.,,,|,, ,, ,.,,..... I . *..,.*.....|; .|I-....-- • , ,.=..-,, • ,,*.-. • .0 • .. _ ...•., n. h,l.,,l ,,.I; 'l"" ;"|",. • "':i=:'P_;: ...... I " ".'"" _'". "|I n'- ,... .... ,.
• hi-.:.. ,*.;,,...:* _is. ,. ..:=.:,. " ....:..|...::,...... " . |.,...•" ' ":';''';'":''_" *X""''''*'' ...... _-.v..l .... i .i.:.. ...... ;....i
• _..:._--_.-.,-*. • .:...:: ...... :: ..... . .... .._..._ ...... , .... v ......... |• -' ...;:i..'=:...i..., .:;.-'h.i...l..... =' .IS;,..; ...., • I. ... l
-. Is.Z._Im,s'_
• TIME HISTORY
I._ _ "_ " "_ • .... "_ " _ .;
i . ['-- _ ::
2_
: '- _,_;,, : '_ -_ "-;:"; • • ._ -_
• . - .... ,., _. ._ ->-..... _- _ --...-¢_
FREQUENCY SPECTRUM FRF_UENCY SPECTI_UM -ii"
-..-:._.- .=•,- :%_,._-
1966005493-048
Meas. No. E12--_
•_l,,,I,,I,.,,,,n,ll,,l*,-II ..... ,t..,h,,l|:,.ti-i, _ i ; ,ja|l.4..,, ,I.,,,P4i.,t,,|,,,I :,,-1.1:1,, ,,|_.,.i.,, ,;t:i-'.|l,,l,, L.I :,' _I' 1,+1,*= It, ,;I,l.l-I,I,;,,';|
• ".h;.,,.-,::.,..,.,',...+,,--++o.t_..£.'-ti,.t'-..i,'''''" +l.r . I"'t '+"+'i"" -'*"<+";+'" En_ne /+I,,l,_l*lli;'ll , "|n': ll;"• i , i ,,n,I, I • ilmln',,ii lal,, l •='.,lil,-" ;,iiiilJlu_t .,&m|............... .................... r""t:.'-:,:",-"'": ....'l'"'v:*':! '':'|" ::1 '"i :'':° "l'l}rrli'";I _'' '"**'.*'* i'i"tll':l'**'l
I. , , n . • ?I •...... ,.;;,,,..L':I-';.'.;.--,,.._..,,..,..,,,_ .,.-,_l-.._....,--.,|.,,., Sensitivity P_wallel to Pu_ Axls•=........_h......4|...1.'';..=*-|i..|=a|.t.il ,.:......-'; ;'I i'4i...._
..... _I''II '" .... I...i..-._...l...|J. i .... |;...-';.i::_{_.ll..m.p....i_ .... t=|li.i=;.==._-i|l.==| iliin;|lin, i=..ua|=i_-' _ .li-'i|.i_.ii 1| "=l| 111"
.... :., ;.*..,:l:.n.:.J.;,:loUll,.,,,,.|,._:.:.,.i; .-v..n_|:oi__..;_a_,'lp.,..,
Location: Page 15• ..;i. Ill..|....|......|...==|.. _.. |.'_nl_1
......: i.! ..... IV....|i|i;i.:.|l*..i.lt_J..;;.+i._i..*.i..;i;.'i_. t...::.is_.!{ :S;i
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•t.. ,l,.T,..+, :| ;.._.la H ..... :'*,',+:'?_4"" ........................,.......'.".."'',.. ......' "._..',;.':-',:'::,I.:_:;'__:,,'k°_:ia+u_.'t;'il:'l;{;;:';l:+",.;ll._i{:t'V"." _ --_'- ,n,- ,,-, u Remar]_,.i•_t;,,,o"_.',:.tl-.'-,,_-t_._,.{:+'-|l.-',1_._;,,t. - ;'-. -_-|'_.t,;*,_-',-'!'-'141- _
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..... 111.11". • |lll...n.ll4...l.l.;.+l.= .111
-+ --..;t++..usi m ._.s.._i!il='+i.h.--Litl'.._ .i--i.l..._..|.{i.'l_l..i-'|. .._- :'l."l.l.'_.hl.;-.il ...|;1;.{{|_+.. l;. ..;.. "l-'.ll".li==ln.. -'.l
•..;t., mm..==|..+.. " "|'...':::::' ; :i.{:;_!::';_::!:'.:v.l:i:':;::;':_ :........i :,:+.;q:L;_':...... ,L'......:_'"':-......."_'",.:"L' ':; ;::":_:"i_.'_:'{':"!--
n_mlm, r"
, TIME HISTORY ""
1
_ Meas. No. E_,-6_.o_
• ,.., ;:.......l,i. """t:'::"''' a;L..; Iw,: .... I-"-% m a"*': e''"
• ..'n ," :...'. "|i''"" .... :, ".'='n|'.':'. |';'"" " "'_.............. •......... ,-', ........ ".-.;.......... Description _ul"bS._ Germ
...... '.,...:::,.':,!;,,i:,.;.:,:.,,,.,;iii .....:..,:.+i;.,: _e 6
..... ,:.',. .... .m,.._.,.,:.._,.,.,..:,.!,,...:.,.i.ii..,,.,.,!, .,;h:,,i,. ,,." ""
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1966005493-052
!
• , - . . .
L Meas. No. El07-11
' .: ." ." ::'i '_i • :'."! : ::::.::.:"-'... '..........." ..................... "........ Description Spider Bear.a w....... i .|- , , .,n.,,. ,,,. J| • h ,| ..,.. o........
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, TIME HISTORY -- i -_'"J
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1966005493-056
. !
I
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.... = -- Meas. No. E_9.-?
Description Shear Panel Between
Fins I and II
Sensitivity LongltudinsZL
e
." Location: Page 19 -"
. Calibration + 30 G
.. _ Remarks
| -
I
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, TIME HISTORY
1966005493-062
%,i
-_ ..... . ............................ . .
1966005493-064
1966005493-065
1966005493-066
1966005493-067
o.
I
1966005493-069
S
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!
J r ,_L Meas. No. E345-80Z _ ,%
:.i.... ................... 7.'..;_._........ ..-....- _:........ :......................_..... ""'_"':-"'"";'"- ' ' " De sCr_pt_on ST- 1-24'Support
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196600549:3-070
Meas. Ho. E346-802u
Description STo124 Support
Sensitivity Tangential
5? ,'I
4 :,.,l"
1966005493-072
Meas. No. E348-802&T..-
• .d ...... ...|.m..|.:l_, .... I:.:..no...tl0.... e.. m .-._
". .... !............. :....... ,.,.....,.,.-'...... " ............:....,.-'.... - .. Description Air Bearing Supply .Mount-.":i!:i _;'.",i:-,t':': !..... .' .'J .'i;,.,:.,.,...... ;.,.,, ................ I=|11 =|._|,= .l_,-.-..=| ........... ==.........
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:" !l:;i',i !|._ll,iii ':', I::':l:i i _,....... ;': ........ ' .....•" '-.... _,_---it:_i:':'..t:-.-:-:"_:"1I| .., _m. ......... ' • _i .... _ .',..'..'",,_ ......'|.i!l"i,. |t." I_11 .'*I" I'-';i; ..... I:...li.,.,,.., I , ..,..,I was not evailable due to commutation.,.i- ..... i i "..:.,d::'; ..... h,..i..:.-'•..:..,_.._.,,.:i:'I _; '.:;!; . ";.'.!::,:_
• I='I'" "'.=:' I;I i(,l*,.l, ..II. "I • .":r|'ll""J "'''.''='="":l:t;'.' "::'! ':! :':::";'.':; "i _11 .... "'":'"",'"" .....
{ "":l"l_l|*; ';_ _ t, _":,l',"i "! ._ ,-,.l"..-'".,'.-p,,--,"':'"":..... ""';';:" _er_ce chan_el dropout f:rol_ _9.• mlpllla I Ill ,m_ ...... lllll • _ Illlllll_ Illi" "_1_ mill
i,, ii i • Ii, I ii1|1, iJ,, [ i ii ,,, J,,| ...... i,, ,i;,= i
..... I'1-. _ "'"'"'i ..... t., .,:]. I,...... ,- I.- , .':- '..l..|...l.'._._- |-.. ._.....i...-.,.."I' |" ",...... -'='""1"'*""_....... ,.., ........... ;....... • ,..-.I....... j ..v.... seconds to 150. T seconds•• .|=.-1 _ • .,-- | .... h ..*, -- . .... _::'' .... ".'" ":
"'."'"L" ';" !:' . ;i-,,;.,,:;,,.._., .l: ; ..,; ,-|.,..;,....::..:.
; TIME HISTORY _
* t !& "'"......ll:l _ : : i _ i [:_ i i :l: i
-=7 [ :_ } ,,.[[: [= ....... IllS .... r. i _ Ill I
| .... ,, : '_1 !!!11 1
" r LT [ ::
[ I _ll,_, ,::
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J i _ [ ill illl II, ' 1 I I llUllli i
l ' L/w/, tem'llt...,., ! ] : _ I I
- i FREQUENCY SPECTRUM FREQUENCY SPECTRUM i.58
1966005493-073
Meas. No. E349-802
,,::.:, ?.: .i. ":i:i:::i": ::'i:::.:.::." ," ,, .1::.." ",..',;.".,_, Description Air Bearing Supply[ ...... . ........ ..... _"
i "L':'!:..':'_., ,:'.::"::::'.:"":'.n
...................... , ...;.,;., ...: ..... "... •: ...' : ..;'' :'::..:::.:':::'..:.. i. : :.. :.... : ,... Motmth_g Panels
• • , ..... i,,,n , ,,,| n , •• , , , " ...... , ..... I ,, ,,|- i,.......... | ....... .... i.. • ........... . ......... _.. •• : • .r n :. ..._ . :. .. ...... -.... • • . .:...
• : ::. :'" ;............ :............. ;'" Sensitivity Perpendicular to PaneliI iii111 1.:11:: ..... 'i I I 1.11 i ..1.. ::1 ; ,;. i111 i:1:1;:_1;i.i1:11. ; i.i ;
' • . ! .... :... ":'-'::i. ":Zh':L: ." "; ;:|" . ............... ,1... , ."• ....... , ...... w • ,m ,,
...........:,..,:.,:.• ::- • .::.::,.,........ .........,.. ,...;.,, ': • ,':.,% '.,'i,_t':;i, (.'A I,: !L._ _ !i(_.N"
• "::..:.-.::.: .... ' " " ' • Z4
....................... • .... ,./" Locat;on: Pagei ,, , .............. i ....... • •
s i• l .... ,.." ........ , .... , , ...:• |; ...... :".: |:'" I" '.': "'"H ..... ;" " "'1";'.. "-:'".': ". "I • _ • I _ ..... I • Im • i nm n n m
.... , ...... _. i ............ J_.'" ". Calibration ± 10 G
°'"'i:'":' ......... . ... i....._;..-.,.._-.:...,-_,-....1:;.:.¢..i.......... ;'i'._._]1" %1 _.! .• . • ., ........ • .... s | . •
............... .............. ,f'":-': ":" • Remarks Igt-Cli_ht calib.Cation atl • , .|. .'.. i. .l • i • , II .... l.. : : --.
... , ..... ,. .. , ....... %.. . " ..,! "i ...................• " . i " ' '" --'..'. ', ' : II.:l ....... J...
:":; .... • ............... - 130.7 seconds....... i ....... | "" • |
j,::.............. #, ........i • , , , • | ,,| , , • ,.... n •: "i: ". : "'. ":'.!" I" . . '. . ' "k. ''"":" ":" I "'''_ " ........
I ";"' ": ,h..,..: . ::. ;.....:, ::. !.. ..... _: ; •
'r • ................ ::/.'!" :.,.;.!:::.:..:' "'::.:.'; ........ : "'; ..... h.;""i.'" .. . :,:.;....: .. .,_. 'l".:.,l::,i,.'. '• • ; -;:7 ............ i ..........
......... , .... ",_.... , ...;, . . ,' ;. ": . " -' .: I.: ' . .: '-::..: . : :."!h,:l ", '1 .: ..'-":• • h , -% ', -- " " '" "' " ' " "" '" "
, TIME HISTORY ,
Meas. No. E352-802
ii t" | t '2" ']'
_l_ !IN-'__ was not available due to commutation.
i Service channel dropout from 149. Z
-_,
| TIME HISTORY :
•_ FREQUENCY SPECTRUM FREQUENCY SPECTRUM!
6O
,-i
1966005493-075
Moas. No. E353-B02_,_ _,'-
i 'i!.:IllillliillJlillll!liMlillii!llllilllllllllllllil_:,_,.'::'.'.:....'"If;If',llIflt_,.illlll,lllltllltitll.ttilllfltttlttt,l_, ........ Description RP Assembly Mortaring
, I +,,+,.....,,.++.+,.-'.'I+! . . t,,i+,,,':,'"I"',"!ifIt t_ ,_ Jt! m+,I
" "'!IiII!+,IiIIIgII_+J!I!I!HI+I!IlMIi_N!II!I!iiI!:., III Location: Page Z5
i Calibration _+10 GI
+'++i@ ..-..+.,.-°,°,..,,...,,...,
i.
130. 7 seconds.
i. _l_t, , I l ,'illIlm i"
b TIME HISTORY
+__ _] t_ + Il,kliii,.l. lilt II'll +ll+I_ _141+. ira. _ If,. _._
marl ............... ,..,
........ _ " kiiii ' 'II_,_'" _ -:..llIII lllIl ,
lilil lllIl'" ::;;: _iiii .....:: Iilli ' ';i:IIll '
......._' IIIII IIIII ":"
I IIII .... I Illl - "._'-,,IIIII IIIII - -",:.'/_
. ,;_.... ; . , j_.i +i _ - -- i__+ ......
I IIII , IIILI ,,1+
I111| llllI: L Iltll ^ II111
IIIII_I+ ..!!!!!i lllll • i i i ii ; ,- _.
I i I£1111 _lll I IIII ! "_'_ _-'_"
I_ tllll II i"_ ll_IIIII. . ....;../ llkI4 L _H_I, +- ,.._
++ ,.+..-
, .'._'!
FREQUENCY SPECTRUM FREQUENCY SPECTRUM '; _--.
i __:,:_•.+%_
6_ _ _n--/-'._-._"
i:'Y.-+• :&Y
1966005493-076
:: j Meas. No. E354-802
• i I. _ It++o6 ,_ + t, • -+|" it • t ++_ _ Roe _,li_e_• - . .I _ I -"........ Guidance+ __'_.'__ ....... Description Computer Support
..... m.t
• .._t_,li__mlltilllt_C_d_.,_m_ _.t_• I l li 10 G
_ Calibration
_'''i-' _ - _ ]_ Remarks Service channel dropou_i.
__te_]___ _ from 149. Z seconds to 150. 7 seconds..., __m__._r_ _!
_14,.Hl,__ I " "_ "" J :1 "
-i mlllimll+ I-
TIME HISTORY •
Meas. No. E355-80Z
•,.... .,...... :.:..:. ,:....-'-'•:....:.:....:....-,:...,-......::::-:..,..-..,. .. Description Guidance Computer Suppgrt
•...;-..:.:.:.':..:".:• : .: : ,. '| • : ... :.• .... :'.',::.".:.'':'.'..'......:..'.:'u'.'.'" Panel
: :. :... ..:, ,............:.:.:...•.:: ::.::[: ' " ....... ' " " ':,A.'.,.: :, • '
: "i."".:,:."'.'", ".: ::: :."".:::" .':"".:'! Sensitivit7 Perpendicular to Panel..... ':&i::[h".::':'..:.:..i:!.:.:!:i':'::::.::.. . "." ..... '
•n.... | .. . , .... • .... • .... n.... • .. I • • • ' ,...... n ....
• w | ' ..... _ ....... , t ":" "'' : " .'..: ..:.1;:.... " ;" " .a,".'... .... : :." "".
'e " " '" "' "'" "ill "" "" "':l''" ""' """';" : ' "" !: .; ...:.._ ' ._....u.. ..... • ..."._..":' Location: Page 26
'" 'm"n ;'_1 ,. ,... n... m.,. • ,."v •: : ', • :,: i:i?_,: :,:i; : . . , : h." :. !'" :.'.' " " "' :
: .... :."......_.'......* ........i..-:::.':'-:.:":.::..::.... Calibration _ I0 G: :..!..:..:K.":I'"" " "::':":'"•,4 '. . '.: "::x. :'.:.!:.''.i
• • n. I. • n 11 • q, ............ • .... i. ,n • . • ._. : ,.J .... 'i." • .., ..,.,....... , ,: : .., :, ...._.;..:!..:,,.:...::.:,:,..:: Remarks Launch environment not"' . " ;_, ;' "" .. "| L',. '.: ...... , ....
• "' " • .... , , ..._ .... ..:*.4 ......... , ........ "'l " ' .... ?: "i;'..:... i_ • _'i"i';i_:.:',";:!:";".'!:"" available due to commutation. Service
'" :/:.i::"/...!"T ....:":"...... ' ..... .'": .... :.. ' ..... I ! :" '•1'1 .t: ,,; , ,,.,, , : ,, .
..... .... :_ :': ::::!"i,......... : : ....... ! ; ,.:L ,. i! channel dropout from 149. Z seconds• . ; , .., .... " .'" .'n "", I.".... . I ..... • ...... i ." .:...
• . ..... i .. .n | n i1_ ........ ,I • '•i :_:.......:.".... ..:::':'|'• ..:',,1":":::....:,'"":::"'" to 150.7 seconds., i , i.... , .... 1 .'t1.,..,.• • , r..---t
........ : .... ' ..... 're.i-- , • ..,.-J • ',
• , ¢I,( ii m
. TIME HISTOKY - ............... _.
1966005493-078
-%
.o,+
I °
, Meas. No, E359_02
:".":i'"'"':":":::•"";:......':':_""'.:,".'.,""'_""• ..1:".'::,'" "...] ""_.:".'i:.!:'::i: :.;{I:..:'.'." ..., ' :'" Description UpF_r Instrument Unit
..... ' " • ' ' ....... |'' I" i .,.. , • .,
'' ,' ................... _ounting Ring• • , • I • • • , •, . | .... i .i • • • . ,..,' . . . i .'..'.. . I. ...... !. ., ". i • •
.................. ;."',...... t'-:: .............. ' :"_'""" "L .....,_." .'..::': . 11%"'. . i, ...,-, . :..:...q:..-;.. , : ," : -r_ __..,* ,, 1 "'-............................ •.......... •...... • .......... _--o._ens+t_vlt_----_- ------,_m.+,_.n,_+..• .. ............ :1 ;:_.",.:. ::::::. - ,..,... , ...'..':.:::.:.4
_. |,, ,, • ,.., . .. ,..."i" .'
............... ,, ,, ......... :..... ",, , _!',,,',, !ii=.,.i.=iI lea.no ...... =i =_i_,. =_ ...... II ...: .,I==1 .ii=l .... i.,l.. J ., -|. ,,, s .... , " ,."
"' ......................... ""' Location: Page 25=- ....... ;.i't ...... ,' |"",'i"'.'"' '|;:' ............... ' ....... :"'""
",.'.! ","., ': :', ." .'t ." ".:::,|" "':'.";'::.',.'::., :" 1:"':" .
.:i:': '. " "i • : " "":" _.: : ""_:::' :,'L": ! .'. ' : "" .""". ::., ....... • ..... i ....... It.................... Calibration + !0 G
• .,..,.. .i. ,..... , ....... ..'=.i.. ,, .......... I...| .. .'• . i • , ,., ; :. . , _,,..,.I,,....1.,_ ." • i,l i . ;. ,,, ..... =' ,,.li
l.,,,in,,,=, ...... n.v,.. , f,.l,.,,,, ..... : ,.;.., i...,l..=,l,,..v,,...., i'..::::":.::'::..'.:..':.:a:::;'.':":"'..%,'"...... !:.'::":",::". : :. Remarks Launch envirornent not
•!i.-::'.':"::':'.':'.;_:::_;:.:.':'.;::;:."l'_.';:.;I..:L'TI'., "',,'".i ava±.'l.able clue to co=_*,,atlon.• ,I .... I,I" ,,,;,,_I "hll '" ", ' ''''''I" " '' .... " .... " ......,'l'l ..... I''I I ..... • ..... ' I" • _, • • l, • ....
' ..! ....... :: -:t.i .................. _ ....... " ............ I,,..i
•""._::_:.::':,.._g':':.:.,:..,::'::', .'":_.:.'.::'.::::1..':'.::':L::.;i,q.. ,..,..,._. • ! ....,. *.,',I ..... ,...''_ • • • t'', "' ", '" •
,?..,.. l,., ....... i.,='.. . . i. l, ._ ,. • • i ...a|--, ,g• • i • •...... is • .I . l t • ..i.. l • . .ran i
• e. ,:,1,1, , i|r=, ....... II.,ll ], , ,, '1_.,_ d_, ''I ' •
. TIME HISTORY
J i_ .L.J lip .L
........- I - "_I cw_ see sls¢ s4.f ,_om_t_. s_s_¢ Ii_ sivsl _•S.4011 ,i.lelc, _ _ _41.i_i# .leJe_.
it I Ill]1
i.--' 'i iilil lllfl_ I1
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I I IIII Illt! -'it
""" i Illll , III1,: ;: """ ! i i._iii-U._. ; !.:;; ._
i ] i I fill ;';= .-lJlll . i 1]'' '..... , ]
, iili, till, -']t-": I IIIII IIII ..... :'f:"::;
' IIIIII llli[I_llq L I I __k " .,i_
i . , l!iiii i:r_;'-_ _ .:,_'_• .', I I I I i i ...........II " : -":_':.{_...
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• i I IIIil l,i#llr ;,+'"l llulli lllll f'l lll_ r ++_.
• .t_
FREQUENCY SPECTRUM FREQUEHCY SPECTRV M
I .ii.5+:65 .t -o
+ ..Q:
1966005493-080
i Mea_. No. E360-802, _ _ ....t,i_ cllq4
.......................................... Description Upper Instrument Unitn..,..... n .... I ...... • .... n .... n wu. ..,m.|-. ....;..-ff..'...4.......,, ... ; .r ..... ! ... •
• n....... . .... • ... .............. . u n; l " .n., ...:".:'.':.'.." ..",..'":.,', ::.::':.': ........ Mounting. Ring
•':'::.:,:'-':':,.':::;'.:".':;";h'':..... :'..":',":':... .n. I. • . .......... • • * •
....... •......."...............:.. .:...." .• ' Sensitivity Per-_ndicular %o ring
•_:..;:.::iii..!i!i:'.!'.:!i':i..i.i:.':_ii_:i::i:::.:!,.'_:_'._::,:":. '.......... ' • : '." .i." ""...... " ..:':.'"," "'" .:':'.......
..... : ." ". ,1 i....,. i...is.... , ..... ,,,.. , • • ,.... *.• . • ....... .} .... | |..,., ._ ........ : |.. ..... , .....
'"' ....'' ":'";'"....._..................:..... ; """ 25: ....T;:'"'"'.........,,.X.....h"....":"r"'::''':::'':'''":':::" Location: Page.... ' "' '................ w .......• ...... • ..'" ,
• ,....... •..,I...T .... .._ ...............! .." ".'-..' ......... ._4. ,.... _,,.: ,., ."...... :,'." • .... -
• ' :::.... :.: .;','_:.:.'=",i'-::-:.:i::-_:_ ..... :-.,.:;':::: ....... :." ,. + 10 O, .,.:::::...:; .:. ,_.. : ..,, :,. !:...:. :.: :. • ..v..... . :" Calibration -
:. :..:;_ml.; :'!1 ;1::.:," :':::::': .'I l:':: " • :..:':,,! ":
•'.'":",_'•"'" "':• " '_"'""'' .'i.......... :•' _-r-_rk_ In-flight callbration at 31.?- • ." ":.;': @.:;.IL: "':/: ;,i ; :.,. :.:::w,,.: .. :i" :".!;:'.: :::',.,
• ....m.I ............. .: ..... m _,,.. • ..... | .... , ..... " •...... _,..,.,.._.._:.,,|,..,, ........ •.... :.........n...... _. ,. . .."::i::;':'::',_ :.'.' .'.:,:. -" :':.':::_:::::,: :'.: ':.:: "_:- "' "': s_cor_ds. La_mch envi_n_en_ no'.
•:-,.i1:._'-.:::!:: ',:-'_-::,.,,.::'!..- -..-..::_-.;:'.-;.t-,:---- ,.-_ ........• .: " .i':' ..... :: -::....:. ::. -'."::;::_ i:':: .: .: .".,:" " ..... ".
, .. r......... ,..I ............... ,_ ................. available d_e to co_'._u_._ion........ "n .n. • . ..... | |..• ............ hi..., . ...... .
'._ ...:|..,_ ..... : ..._ . . ; .... ||.,..,h.L ... I :..,,..| ...............
I" "J .............. : i ...... |'" ............ '..... , ......; ......:.... ...... ..I.,. "'1":" ' ''"" ' '" " ' "• "::_:"'.'.'.::.:' ::::". : '." .::.'.: l'_:'::,:;. '.... ':" ':" .: ": ..... _a.. ...... i...,|.. .... ..L .......... |-... _...... l...', -..,| .........
'. .. a.'.v....I... ! '....,. .... ; • ,_.: ....... '_.-.; ..... , ..... ,r-.._
" TIME HISTORYJ •
• ,_:_--_ ---i . .'.. "." . I.
.J
,111| _ • iiii ,, |11|!
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IIII
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: : I I II " II VVI ' 1,
,,_, ,.-al4
"l mmmm _ _,m _-
Q
FREQUENCY SPECTRUM FREQUENCY SPECTRUM
66
1966005493-081
1966005493-082
-_- Meas. No. E362-602
........ '.. ......... ;.,:l ..... ;,..,: ...... ;.... ,-'_",.-.. '- -
..:.'._..'.;.',.,;,:..::,'.'..'.:...:..:_!.,:._.,..4;......',_""i........ D_scrip_ion Lower Instrument Unit- ......'...i ..... ,..:,..,.. _., ,;:...| !.:i,,,.._.-,...;....'.t."" "'.'.:',
, .:! i .;.....,..'.:.. :...... : :e.'.,,:..," '.. ,"_. :; '." ' ........'-_.... "_--_ Rin_., |...,_', .,'{._,l.|,.;....Ih.,|i,:.|,:-i.|:,.,4..:,|i-'.;--''li"''J';':;_ ""
• • ' ! .. I , I '. ' • ' ! • ! .I.1...•"._':::r:.'-'::r:".:. :':,;",':-'4i.:.',.'.,h,...-'.,;:::,.,..',.'-..;.,,, .:'..
• ..:...;li,, I .... ' .... '._l":"'il" ;'*'""" "."".| ........... Sens_tiv{ty Pez_-_ndict_]PJ[• to z-_: i _ " : ' " • " ' • .. -* ..... i i......_...._:..'-LL:,.. :8.: ...... L..._.:'T., L'..':.._i-.-.*!*-.l:.. :.|:-.:" :'"" :*'...i.,.::,.4.1,i.,I,..,,....,.-'_.! .I;I||.,,.,.,, ...... ,..I,..,,; .... .,::-.
......... i, :,,|, ; :,I,..', :,,,. I. './= .'--"-i.i., |=.I, =' -"I..,-' •" l,,i.,l;,,,.,,=, I-.,• ,',.,..,,,._:.,.!, :.,..,,;_:,i'l,/_,..-ii,.l.,:.,!L_.:'|,:,:.h-,'t ," ,! ,_• .l;-',ih..l;,.-'-|ll,il.-l-ll ..l.'*||llllli|li .%1! l|"Is ;';i':'"":ll""
• il .=i|_&_le=.ll . ,='-..=l.{.,l,=ImJip-'tlii{.li_l_ll_.w=.'illIA_l=i_IA._=_i_" _=:.".i;I=*",'.,,:,,;,, s';,|,*..-'i=!.|l,l-'.,, II ;:,'li--l,|,,,-, .=";I';"."I''"";"I.,I.,..:..,I,...,.-...... l:_'-"t':,'!_]',l':,'l."."l":'l:"l":"l "'''l:" Location: Page 25
.,I.,, ...... lel;||ll,|i,,_-i,, ,4,:-'t|,ll,I; ..... ;,!''" |l|'l'il,'ll'| "_:"•I'.',.:._: ,,!. :..L.', ..I,'1._: ,' i, I'",| ':IL"" 1"_;! :'.' _'._'"" ::';' !''"" ""_ _""•i|.l*.**,-'.i* ..... ."l.'l's4*l*'l";'1" 't:l:_.;"*|':""'"'.".'- :': :,': ..... ;"" F 10,,:l"'LI;'::ll":"'"J'l:_ '''" ;"i','"'l_;:'"_';; :':'.';'"',';:";'" ","" Calibration --.l,l,, |_e,l-i:l,,ii,|,_ i..__,,1_=., ;,_1_ i,i;|_;._, i_, ,a,_,|, ,-| . i,|=,,,,,,1.,;,,ll,,,.l;i, i_il..i,;|_j_lli,i,;ll..al,l|,_,.,i,,.,| ,I, .,; ..... ,.,,|.,,,:.,;•.|" "i,!;'!';':};.','_.,,!';l'."i:'.{_li'_;_;'"'l'"! "_";'"'";=':'"I"';•'il ..... "."-.J,,' l_i'", ....... ,";;_'_1 't' .... :" ""_'" ...... l:'" Remarks
.t! '"l ...............'................. " %1 • ,,, .,,,.l..v' '.'lff, • , ..'1.,. _:.., .:...........,I..,"',......,I.....,.,.!..,.,,.,*d,:...,..I....,,,•.'" :,o-d'":....ll,=_. I|,l.:#|v|t *',I'.'I _! ' l I'" Ill :" !."l, .-,,-,_**_'i._ ;,!-:"' ;"'.._lll:;:.,, ll:-|,-.l|_l-*.;It,,"l'il |" !i' I'I" " I "ll'i""l..'"
:"i;:':,:!.,l_IL_:, _,.:--..-';,i.'::h:.;.-',Ni, !;:'i,"::L'i'i-'-'"'"•:_t:.:.:..i:.;;l_ .,,:.,,,..:!|_::-|i.:.ii_.;;;_ • ",;..... :*"'."..... ':::
-.-I I,,,I,,,. i tr,_-,'- A*- ;--,|:-,, P*,, ;,l"|r';: L_" ."-';; ............ t!" ";'",'1_;_ .... I :'':i| ....... "";:;::'"" :" "_;;L':""-'.:-'.,,',L,I *''1 .... i --I!1111 ,-,,"'-_,":'"'- "li'"," • • ,' • i|.,- I-..'l,':;t-.--!:,-,I,- t..... |;,;|li'"',:' .s_'l.:.,i , _,,.._..I il "_1; |&l''ll IIIIII I I I |ll'll';= I ..... I1_11 II ...... Illll, , I I s,' .' '.i, ,I "h,*.'. " . .i . ",..-:.- --,.=..,
TIME HISTORY
"- _ ..........' -_ _.... "--:-__-_-_-....._ ;____ i.... ' I''' l [ i] I , _',1 " il
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---+-+---+H-_ I 2 .....____j__j_,!!!
: -- T-T- __ " _
_ FREQUENCY .°PECTRUM FI_EQUE;I_.CY SPECTRUMI•, 68
•_" .
1966005493-083
If
!
ie
-- Meas. No. 1379--°02
_r._ _.ud_vaZ
I;|':L:_._-_'____.::__._ :.::::::::_:::_:.;_Nj_::_ Location: Page
:_._4_.;_.i_::::_ :_:-::;:=,,:__# :-.| Calibration -- ""
,. .......:::::::::::::::::::::::::::::::::::::::::::::::::::::::::::: av_lable due to eor_=_atlon,E._
_i;;ii_;_h'gilgiilgi'_}g-'-_,;_.iiiiitiiiiiiii;_ -_Z_
TIME HISTORY
L
.... ---........... _Z; .....e,m_.,m,,
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| I | i ! ]i I i i I --|_ i I ; I #i:: i [ i iIill I !
.....+ _ _ iIIIII I I I IIIIiI-_I=.i'.--_."F-:_--_-,,-:-_n'_r.---____-_,.+i-----t= ]......k_)L__._LM_i_._._TLT_L_iiii;i--i,i
: r I i" I_1 ' ,... , i _,iliii! illi!_llii _--__ __i_;=-_V_=-+-_ --, : "' t- _-4"--i-'t-f-,H_ ::!, | i i , I I II :_: l
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.=I /I I!lll!t I I_t|lll 1 ,.,_._--_.-:-__:_I :I I I flit II :: i,_l:ll I IIllli :L.I:-I ';:7':_ _ ". '- ." il I I IlI II ", _-_..---i-P-H-H.'if._.,, ,,,.: -=zJ'_. i ! .11;ill %t II"1 I!1111 IIl'lilii
._' i I11__ i I III!'lt[IPllli .tllll_ llllt r- llllllll • ,o
FR-_QUENCY SPECTRUM FRI_-Q_ENCY SPECTRUM
69..
:. _.
1966005493-084
- Meas. No. E380-802
!_':iiii_i_iiiiiiiiiiiiiiiiiii_iii_iii_iiiii!ii_iiiii_i_iiiii_iiiii!i;Description Upper Instrument Uni'c
.. ==========================================================================___iiii__L;.:.i_iii_iiii'!L:L.'!:'!iii-iiiiiii-iiiiii;.i____, ___..........::,,._
..__ Sensitivity Perpendicular to ring
Pa,,e 27
Calibration + 10 G
Remarks .Latmch ev_vironment not
a_a_iable due to com_atation. In-fLight
-_" calibrations at 31.7 and 91.7 seconds.
=
TIME I-HSTORY
.,. .--.;_ _.:-
--_ ii!_ ;,.... - __'-'_"_'!1_ _-_, ii i_ _l _ ...._=____:. : J -'-==FT-4_4_;i : : ::;_:'": , , , ,,iII|
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• • , . ii _ _ I__U_-_I E_ .'/_I , I _I ....I_
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' '"'"'"-" ffTfftHLIiX¢{i f" l " I I Ii Ill "111_I.. "_-_I - ' .... ''
_i FREQUENCY SPECTRUM FREQUENCY SPECTRUM
70
1966005493-085
_ Meas. No. E_J81-802
_::.W__.__:_HHH ........................_- Description Lower InstrumentUnlt
_ I[:2"_-..,,_::-_,_-FL,GnT C,,,JuRA IONf_,n|,.._ Youn%ing Ring
'; " ::':: _ l.'h"..';"..: ".:"" ":.;._.:.. : ".: .:.,..:.4.._:::;::".-"......u,'::i""...... . .:'.'#....: , ,,., , • ., ...""
: • " "': :,':................i i.I "" Sensitivit7 Longitudinal• • i. 'i :'"."::'" : : i : ':.k...i.':" i "':.::':::.'::": ",:; ...... ,. • i....... . :. • ", _r. ".
•....: I. '''; :_"3: :..... :;j|I BB
- ,. ":'".'""" " ,;':..... ;":;...:"::..:'."!..;'I.....• . ! ..... !.... , . , ,i ,.
.................... • .... Location: Page Z7:. , • "" • '" I I .. a "" '"IP'_'"" .... ;
• , -' ,. • I ....... ' " " ,." ,'." ." : . + G• , .......................... _....... ... . . ,• ; ..... : : ......... Calibration 10• . . ..: . : , ::.. : ., .I .... :, ........"'" " " " * | " | "" L ..... | "'" ' '"..,, ....................................... "v "" ......".":. " " • "'" """: ::.....":"!',t.':"".:;" ..: "::.'v',. "'i • ; Remarks In-flight calibrationat' | J .'" ' " • .,! • • .......... I),......
"' • '" ':' : :' ":F' :.': '" .:'..-'.:: ,_':':'..:!':':" I': ."' "'"" ,".:! .... : ....... .. ..: .:.:, ..... :: '_:._.....: : _ ....... . .......... _ .... I_0.7 seconds.,..................................._..........; "1 .............• ,: : .i ."' " .:.,: : " .'% • ::!.'. Y:' • "
.L ... ,. ::...: :.':..: .:::..:'.. ":t. :...;,L.:..'..'. ....... :o • ... :-.. , -. :. ::-... ;:',':. • '. .. ,• ; • . :., _ ....... _ %: .... ( ......
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I ..,.... ! • | • * . ....... I ....... | ......
•( ,¢me
• TIME HIS'IORY
""" " "..... Ib,='.z=,- ......... J . .........• _ .•.......... "....." -_ "" : " [:;'l:'iii....i,, i::.i:_i;_:, .__ -.. ; ;;_,_=..... 1;;;; ""
_----_ !'" _ ;',q _ __t i I,,,, _1 , ,,,,_
,III_II ....; ...... . _LLIII . IIJill , -I i-!iillI|_ I | • if 2 } ! I I } _ l I I_,,,, [ _,H,; I Iii Iiili r
_ ilL] IJlll r_ IIIII [ I!!11 i _IIIII --
-' "III I!IIiI!IIII.,, -"_o4 I j I |||'' ::1 I | | ! "_"_"
i:i i]lli "- : t;l_l :l _l:lJ ".
-"'_ i "i :i: li:iii;-l;ii : _i!l ,s{_"" r _ _ _ _ /_ Iul I 1 IIIPI ' ,111| t I-II :;"
.. /1_/ IIIII!!._ i llllJ:.ll._,_IIl_] ....go ,NI_
FREQUENCY SPECTRUIVl FREQUENCY-SPECTRUM
71 :" .._.,;;"._.
"I'-':, " " "j':,}•;....'_'_.:-". ,_;,._-
1966005493-086
,......L Meas. No. E382-_.02Io if. • sl_
• :'":: ..... :.'".'.:', :;'"':" ,.'."Li".V :.';" -% . .',......,. L-. ..... ......" ...... ;....'..'j ...,....: ....... . ..... - .....
............ :...... "'"',! ........ .'.': ":...... :.... Description Lower Inst, rument Ul__it.... '"'|' ; "" ..... ; ' , ............ |....i ...... : ........• • ..... . ...... -..'..:'..::: ..... ,. , ........... , ............i.,i ..l.i. IIIII.LIII'4.'I_III "I ..IiI:I.VIIId..." II .III..ll',:.l_'l _I
• :;':.':': .".;':::::[. :'.,.:...i.. :-'" ::::::::::::::::::::::: ::'"':;'.::': IIount_-ug Ring,"" | , ........ '. .i..' .....I ..... . h: .... '" I "' ""• ''''" '' : ..... I |" e..,,,l.,.. ,; ,..,1,.. I • ,=.|..,'.:., ' •
• , , s.. '1:" ,''. ',. ''," .-. '. ; ....... :..S,l,ht; .... "., .,; ..
............ , ............... ;'' '........................ Sensitivity Per_endicLLlar to ringl..," ,| .,. .., .... '- -" .: ..., ..... ,L...-' ..i,." .,.-',...' "..,.
• ..... i.'..'... ! ...... "| ..... Iw.... "': ....... ,..".. ":..-.I..,'-'.-I ' .... ' " ";.''"" "I'''";'"i i .i.-.-',, :,. .. -',.--'..-, ,.., ,! : ..[ . • .ill ..._ll ...... .. • .J • I .. , . ,.1|.'.| .'.'.
• • : ..... ,.... ...... ..:'.j:....:...,_...., ...;.. : .......:...... ".,l... bZ7..... ".:'...... !:,;,,., .... ............ ;.,, ,': ." .. Location: Page
• lliI.,ll...,..... _ II.I..,IL , |..h 1''" '' I'''II''' "'i''''" | ,I..I mlllmlm I i,II I_lml_. _ ,I, I ..... _,1_ ............. i,,lIlamll lira
I I'l'i'lI'lll _11'' I ll'll :;''l&''''''l'' I''''1," I'''''; .... ; .... I" ,1'''
iI=ml=l.mi=l_ i.iI=..l .Imiiii ii= iiI.= iillm_•i' I mlm=l fill m :.... _I•I.I,. .......... ::.,..,:i ...... i ......... ._.., ........ , ......... ,....... Calibration + I0 G..i m..,, ....... , .,|., n-. ,im..,wo .... wJ.. , '....-:|,|.1,. ii ......."., '..; ...... _., ..I:," .... ..,...-....... :,:_ ...L;..'..,:......... 'i..... '..,-..f..,...,.;........_....: ..........,_,.,,..,., .................":1.......... , • ".-'........ q ........... ;it: ..... ! ....... "' Remarks
: ':::i:;_;;:::;::::::':_:;:;':;F::[':':'_':!''l:i!:'''!:i:':_:_:=:':':::'''':•" i ............ ,"_':" _" ;" '" .; " : .'. ;: ..... ;" ' ";:'.' ......•'r ",:'" .,,,,..,_,.,,:,l., -t,'";:,,l:,,= :-',- ,if,, ,,: :,: "I .....
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,' ,l" T ::"!; ,'_ i"'-", ,'" :q.',.' ""." h ........ : ..:; .... ,.
.! ........", m" ,, .. v." . ' I.' . "--" . ';" ." ;."".'";."
1966005493-087
:, Meas. No. _369-.¢_
'" "....... :"::";:.L':':;':: .... ":::" :':'.'.'.." :: - :'-'.''"......... !T_er". .......... " :';.::,'..'.-.:':;.'-..: '-.":.." .... Description ::.-t ,',_-.'CI:otmting ....
: ] .:,;. '..';_...:::";.': .'.," "i. " • : ;'.,'; .::":,• ., • ...... , ,.. , .... u#, • '
: _. : ......... •...... .. ..... :'. :"::." .... :'.:i ,v,_._.,.T^_^_ .'e_vmm
"i .......-. .:: .:';.i,'.., :;. "':' ":',:':"'; , "";,'",:. ::':;: "....... n., ," .... ' '" • , • • : • ' .... |'" • •
nn .,. , ......... I..D ,, • ,' ......... 'v .... ' ......... ! ..... "'"• . . , .m.. I .,. , . ,.. , ,. , ,i ,. , .... ,,.................. , ............... Sensitivity Lon,-_ _udtnal.• . . .. .i.:, . -:'1" t"" " " • " • "1 .... : :I
,'." "'." :.'"'_:,_ ".i :'::"._': :':;":":'.":" ;: : : :" .... ".m m
........ H ..... ' • .t •............ ; ......• • .. ,, • ,i . ,, i • , ......... m ..... , ......• ,,,. .... ,a,i ,,i J[ ........ a,,aa||,,, ,-ml, ' 'te-,l,l.a ,,,11. ....
;' ' • ' .'._r • "'1''1_ ' "'' | .......... I . . :• • . ,n.. . I ............. : • ,, ....... ,:,,..: ,',.. :., ........
•,.................. . ....r'"',. . . ', ............... • ......;'"'_..........., .... .. Location: Page 28• I . .; ....... , ,l..,.t* ;,...i .... ,.,n ..n.. •i:"" :':,.".. ;,. i ......... ",,'..t, •
. ., ::!::.: ;:::::,:::: .::,.:..::.::;::::; :::: :: ::1.. ::i ::i::;::._J.,:.:":... :.,::,;._..:.::!i:: .::_:i..!:::'!.':::'::'; Calibration + _..Cr.... • ; ...... .' "'l",'"'" t, • ,,n.,, ,n.:,.,,,- l,l" • .,,,-.h,,n,.-
t ..... .j :;.., ....... t ..',|" .:...,.. ........ .., .. ., •, n........ ,. n,| .... n. ..... .,- n , .: ...... I,n,-,,, . ........• ........ •...... r ......_.............. ,L......................... . .... Remarks
t • , v • n • • ' t ." .... . ......, ........... _..................... i_,,.,,.,,. ................ :• ". tli=.|..;,,mt_|,,J*,=.4- ..,-tt,:...I.,. "V'; f_...,,=,..,.|..... 6.,,.t,.,,.,l ...... ..-...... F ' " :"-: ...... , ,'" ..........
| | ...; .,,. . ,...., ..... , ..*.,;.., .... ,t,n., ..... . .,.: ,,. ,,ill I , ...... ,..l.....n.. ....... ,.,. ,........ ,,-;., ...... ,........ .',,,,o.;...
• .| ,,,,.., ........ , ,., _. • , • t, _ L ,t ,. ;,., _.;,,,-.,.....,
,, i ....... ;4.... ,,.....,.. .... , ...... "1..., ...... ,..,,., .; ..... ;• ] • ..ll.. ; • . . ..,...,..: ..... | [,_., ........... ,..i .:n I • =. ,; .., .f. I..,..,.., , -t., • • ," .... ,..a_;.. -n..,l.-. ..........
• ' ..... _.,..,t4...,,...,.,.,.,i,. l,,,=,i.....,._..,:. .,_..-t.*, -'-,n ",;.-a.r_. • ,, s • ,..,s ....... ,;;-.|.,....,..'., ,._., .n".. "' ," :,r_ n,.... W4. . ..t .... ,! ,. • .,.,.n.,.....=.--.,.|_=_.., .,,:.'.. .-
' • t • • ...... I." ....... "n "'"|" "In n'w,"" i..u_mA',, ', n'.,• _ - ,. M N . m _ a • • n| . ,. ,,* ,-
1966005493-088
74
1966005493-089
-- Meas. No. E971-900
.,,..... :"!: ...."" :',_".... ::"i-.' .......[:.....:...:.........:...........:;,.,.,.............:, Description Lower I._CMounting
. . " ." . . . • . .. .......mm_'.m [. . .. ., ..: .. •
! . ., m. , ., .... : m m. ,.. :..: • : • .......
¢ .............. ........... . ....: ,. "-----_n_=on #6" ""...... !................ _' "i ":........ "'"......... "
.." ..... • .... | • : .... .. ,. , ,.. ... .... ,. •I,w
........ ; ">_"'""": ............:'."'; Sensitivity Longitudinal• • ....... ... ,_ .... , ': ..... . ",..... .'"' ..... " .... .' ,# .... t........ ' ...... ' . ........... " :, .'
' • I'"" "...._........ :.... h :." ",.! : ;i",.|.. :,.
.......... _" ._i. .%,.. "'" ':':..... ;"" "' """'; I "" "il''l'" '" =..=.: . ........ ....h.....{
-" ' ". '_ ;,".' • ",.....:'":'".... ". • ' Location: P/Lae "_"-_..... ) ...... .. • | ...... ; ...... :, ..;." .-:.l !
: ; .......... ,,..,: ...... :% • ...,.,..';..:...' : • • |. A • " • ,., • .. : ..... • ..., ..... ! ",f :'"w. :. ............. ._ .,.. ......... ,.: ..... Calibration + 10 G'i • ". I J. . . • "...,.1": ." ,..,1 ..1 .. ' .;.'. I,...
. • |. • . • . , . . .
................ ............. .......,' ,a ........-".,:_:'"'"...........:':""':' Remarks Launch Environmentnot." I _ • . . . I. " " ", .: ...,... ..d .... :......... ,.. • ...,.| .;.. • .,. , • .¥... |....... • ._ ....,,: :.......! ..
":.....' :':'.......::'";i:! "!"......#".......:;',;":.,.:...:..,......i_ : _. ,..:,:...'q.:.availabledue %o cc_mutation.I . , .. • "..• .t • ...a ' .... . ......... • ......, .... . .... |.. :-" r ....
i., ir , "...'.. "'. % • .. • .,.;,-.:,..' •• . | • _ . . . _ . . , ..
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i rtJ'i'_-H'H!N-HI,H+HII._I_,IIII,','].i]IIN'I+H_'H._._'_IFI"I',
|, ' _- "IIIIIIIlIIIIIHIIIIXIlIII . i.,•. !.I ................. I'H4"+ II Calibration -$ _ "_'""'#thlfl#P,_,_............._!.._fit.._#_#Itt. '°_=:. - _ _1111111111[ - i ...._[_Bl+m_. _,+m_i-_,,,_.''.v,:_ ,,4.1:;:I:_W.,._[I_._I I r[lll I I I I I IIII I I ; i II11_1 ! | I III I 1 I rl I I 1 I I I il I I II I • I Ijl_l_,J,I _Id pt • !
.................... -"|'_It :.-_.
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FREQUENCYSPECTRUM
!=: ......J ..............I
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, ilii-1_,___25_/;_<_t_ .... ...,....,.........._..,,.,_,t_l ;_:_1_:1..... _ -'_L__,___h_,_..__, ._._ .......4 ::* _........_i.r , ..... _. _,.F__.,_.:].._:1..-1._:!_!, • . ± - ,..... ,,,, . .,."i J".ll{_ TIT :. ,._--
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T..r:.T_T,.T4..r____,___(__: : __!, ; _____ __; ! __:- __TTrTI'r_'_.'ITTIT- :" _. "_- _..__..,,,,,,,,,,.,,,:,,,,,,,,___:__-.,_rr"--:b f!__ l_i i_j_: -._i ,! n I ! Illlll li I I II l I i II I I I_, ; rli/It fill fill" i II1 ITJ1 [ '
k"}_.,'_" '_"_"v_" ': ;:'' '_4£_t_b_;_T ' _ .'_,_,-_,,_ r:,,,, _,_'__.1_'_.. ,_,;,,.-,;:,,;,.u_:,,,_.,;,,,,,,"n_.zn'er_',_'r_T_, ............. i
FREQUENCY SPECTRUM FREQUENCY SPECTRU_ ?. ":
77
1966005493-092
t"
Meas, No. ...w_,.-/,. .-•l • . .z. . |
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Ii:L;.l':':..F .... "B'T:I:"I - ;rt'-'l.rl'rr|°."_l-'t•-_
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a FREQUENCY SPECTRUM " "'-
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J 96600549:3-094
Meas. No. i,66-802
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TIME HISTORY
_. Meas. No. L?G-900m._ .:!
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• TIME HISTORY
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FREQUENCY SPECTRUIvl _ REQUENCY SPECTRUM
81 "-,
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1966005493-096