guidance and navigation - ibiblio quarterly technical progress... · figure 1-1 shows the current...
Post on 05-Nov-2019
6 Views
Preview:
TRANSCRIPT
pprove
I
?
DOWNGRADED ATP INTERVALS : DECLASS- AFTER 12 YEARS .
GUIDANCE AND NAVIGATION
!d 4 b Date g//y43 MILTON B. T R A G E S ~ R , DIRECTOR APOLLO GUIDANCE AND NAVIGATION PROGRAM
ipr ove d
DIRECTOR INSTRUMENTATION LABORATORY
(Unclassif ied Ti t le )
REPORT’E-1389) 1 /------ ( QUARTERLY TECHNICAL PROGRESS REPORT, -.
P R O J E C T A P O L L O GUIDANCE > NAVIGATION PROGRAM
>, P e r i o d endedoune 1963 1 + r ? w a L I ? J.”
I N STR LJ M E N TATi, CAMBRIDGE 7 L A 6 , h
COPY# $0 OF 2)SCOPIES THIS DOCUMENT CONTAINS 52 PAGES
ACKNOWLEDGEMENT
This r epor t w a s p repa red under the ausp ices of DSR P r o j e c t 55-191,
sponsored by the Manned Spacecraft Center of the National Aeronaut ics and Space
Administration through Cont rac t NAS9-153.
U. S. C . , Sections d 794, t he t r a n s m i s s i o n
o r the revelat ion
unauthorized pe
y manner t o a n
i i
PREFACE
Th i s Quar t e r ly Technica l P r o g r e s s Report cons i s t s of the Milestone Char t s
cover ing the schedules for all components and a s sembl i e s of the Apollo Guidance
Equipment , toge ther with comment s or a discussion for each char t .
T h e r e is a l s o a tabulation of a l l meet ings attended by MIT/IL Apollo pe r son-
nel.
The r epor t concludes with a bibliography l is t ing the r e p o r t s published by the
MIT Ins t rumenta t ion Labora to ry under the Apollo P r o g r a m .
iii
PROGRESS SUMMARIES
BIBLIOGRAPHY
TABLE OF CONTENTS
Page 1
3 6
iv
PROGRESS SUMMARIES
F igure 1-1 shows the cu r ren t del ivery schedule for guidance and navigation
s y s t e m s t o be used in the Command Module. A s noted in l a s t month 's r epor t , MIT/IL has d iscussed a proposed change in the composition of Blocks I and 11, which would
m a k e AGE 13 the first Block I1 s y s t e m (Reference MIT/IL l e t t e r AG-302-63, dated
23 May 1963).
f o r m a l approval has not been rece ived from NASA.
F igu re 1-1 has not been changed to re f lec t t h i s proposal , s ince a
F igu re 1 -2 shows a proposed flight t e s t schedule fo r the command module,
giving the al locat ion of AGE s y s t e m s t o a i r f r ames . This proposa l was presented t o NASA in May 1963 by MIT/IL and is documented in L e t t e r AG-382-63, dated 23 May
1963.
T h e philosophy underlying th i s proposal i s ou r d e s i r e t o sh ip G & N s y s t e m s
dest ined t o f l ,y on f l igh ts SA 111, SA 112, and SA 113, f r o m the fac tory a s s e m b l y
point d i r ec t ly t o AMR without passing these s y s t e m s through NAA's facil i ty a t Downey.
Scheduling the de l ivery of G & N flight sys t ems in th i s manner accompl ishes two
impor tan t object ives:
a) It r educes the amount of shipping and handling which flight
s y s t e m s m u s t undergo.
It r educes the accumulated AGE operat ing t i m e p r i o r t o flight
f r o m approximately 1000 hours t o 500 hours . b)
F igu re 1-3 shows a proposed LEM flight test schedule , giving the al locat ion of L E M Guidance and Navigation Systems (LGE) t o LEM vehicles . The proposa l was
presented t o NASA by MIT/IL in May, 1963, and is documented in L e t t e r AG-382-63
dated 23 May 1963.
T h i s schedule was der ived using the s a m e philosophy as that contained in the Command Module Flight T e s t Schedule, F igure 1-2. T h e LGE s y s t e m s dest ined t o
fly a r e shipped f r o m the f ac to ry assembly point d i rec t ly to AMR fo r instal la t ion in
the appropr i a t e LEM.
5, 10 , 11 a r e used.
a s p a r e a t SWMR.
7 , 8, 9 , 10 and 11.
T o check out t he LEM vehicles a t Grumman (GAEC), LGE 2 ,
LEM 3 is checked out a t GAEC by LGE 2 which then becomes
LGE 10 and LGE 11 remain a t GAEC for checkout of LEM 5, 6,
Figure 1-4 shows the de l ivery schedule f o r all subsys t ,ems contained in AGE 4.
T h e t a rge t date f o r del ivery of AGE 4 t o Downey by MIT/IL has been changed f r o m
1 5 October 1963 t o 15 November 1963.
The objectives of AGE 4 a r e as follows: (Reference Apollo P r o j e c t Memo No. 575, L. S. Wilk)
1. Demonstrating the p rope r operation of t he Apollo G & N as represented in AGE 4. Demonstrating the p rope r operation of the G & N GSE.
Proofing of t he pre- instal la t ion AGE t e s t p rocedures .
Proofing of the MIT System T e s t Labora tory facil i t ies.
Proofing of the MIT G & N Labora to ry a t NAA.
Proofing of t h e MIT G 8; N Labora tory at AMR.
2.
3.
4.
5.
6.
F igure 1-5 shows the schedule fo r AGE 5 subsys t ems . A slippage of 3 months
is shown in the Wiring Diagram a n d Flight T e s t P r o g r a m caused by lack of a p r e - l imina ry miss ion profile f rom NASA (Reference MIT/IL l e t t e r AG-357-63 dated 2 7
May 1963).
change i f approved immedia te ly w i l l c ause no fu r the r s l ip in t h e del ivery of AGC 5.
IMU-5 i s shown 6 weeks behind schedule.
with old s tub shaf ts , and retrof i t ted when new units a r e received.
AGC 5 is shown 8 weeks behind schedule. The r ecen t mechanical des ign
IMU-5 will be a s sembled with 16 x r e s o l v e r s
F igure 1-6 shows the del ivery schedule f o r AGE 9 subsys t ems . Under existing
plans, AGE 9 is the f i r s t G & N s y s t e m in Block 11. However, MIT/IL has recent ly
d iscussed with NASA a proposed change to the composition of Blocks I and 11, which
would make AGE 9 a Block I s y s t e m and AGE 13 the f i r s t Block I1 sys t em.
MIT/IL l e t t e r AG-382-63 dated 23 May 1963).
(Reference
AGE 9 is cons idered t o be on schedule with the exception of AGC 9 which mus t
l ag AGC 5 by at l e a s t 4 weeks due to l imitat ions i n production and testing.
The schedule f o r Guidance Theory & P r o g r a m m i n g is shown in Fig. 1-7.
effort is considered t o be on schedule with the exception of t he mi les tone event entitled
"P re l imina ry NASA Mission P ro f i l e Required f r o m NASA" which is requ i r ed by MIT/IL
f o r ana lys i s and prepara t ion of t h e flight computer p r o g r a m s , but which has not yet been received.
27 May 1963.
T h i s
Th i s sl ippage has been repor ted t o MSC i n l e t t e r AG-357-63 dated
F igure 1-8 shows the del ivery schedule for all guidance computers . A s repor ted
in l a s t month's r e p o r t , a new mechanica l des ign h a s been proposed fo r t he computer .
AGC 4 is functioning as a computer i n the l abora to ry at MIT.
AGC 4E3 is shown approximate ly seven weeks behind schedule.
AGC 5 is cons idered to be approximately eight weeks behind schedule i n terms of meet ing the schedule del ivery date , due to a n expected la te del ivery t o MIT/IL of t h e c h a s s i s a s sembly , d r i v e r s , power supply, and misce l laneous components.
The IMU Development P l a n is shown in Fig. 1-9. T h e r m a l tes t ing is continuing IMU-2 w i l l be rebuilt with new stub shaf ts and vibration tests wil l b e r e r u n . on IMU-1.
IMU-4 alignment checks a r e continuing.
IMU-5 will be a s sembled with 16 x r e s o l v e r s with old stub sha f t s , and retrof i t ted
when new uni ts a r e received.
IMU assembly drawings a r e approximately 50% released.
F i g u r e 1-10 gives the del ivery schedule f o r a l l PSA Subsystems. PSA 2 is about 2 weeks behind schedule.
schedule. four weeks behind schedule.
documentation is repor ted t o be 5 weeks behind schednle.
PSA 3 (MIT/IL breadboard) is cons idered t o be on PSA 4 and 5, under construction by MIT/IL to c l a s s I3 documentation, are
PSA 6, under cons t ruc t ion by AC Spark P lug t o c l a s s B
F i g u r e 1-11 shows the del ivery schedule f o r CDU subsys tems. Six CDU g e a r boxes from AC Spark P lug a r e undergoing l abora to ry t e s t s and checkout at MIT/IL.
CDU's f o r s y s t e m 5 a r e repor ted 2 . 5 weeks behind schedule.
In May 1963, MIT/IL i s sued T D A-147 to AC Spark P lug call ing f o r del ivery
of 15 CDU's to the schedule shown below. AC Spark P l u g ' s cu r ren t es t imated del ivery
da t e s a r e shown adjacent t o the scheduled delivery date.
Quantity Schedule ACSP Expected Documentation - Use Delivery Date Delivery Date
8 / 1 / 6 3 8 /25/63 L e s s than C l a s s A Optics
91 15/63 101 16 / 6 3 L e s s than C l a s s A Ine r t i a l
101 1 5 / 63 10/19/63 L e s s than C l a s s A Ine r t i a l
10 /15/63 lO/ l9 /63 L e s s than C l a s s A Optics
11/ 1 / 6 3 1 1 / 2 / 6 3 L e s s than C l a s s A Optics
1 1 / 1 / 6 3 11/2 /63 L e s s than C l a s s A Optics
11 /1 /63 11 /10 /63 C l a s s A Vibration
F i g u r e 1-12 gives the del ivery schedule f o r t he Navigation B a s e subsys tems.
Navigation B a s e f o r AGE 2 is about 2 weeks behind schedule, with del ivery expected 1 2 Ju ly 1963. Navigation B a s e f o r AGE 4 is about 3 weeks behind schedule.
B a s e f o r AGE 5 is on schedule.
Navigation
F i g u r e 1-13 shows the del ivery schedule f o r all D & C Subsystems.
board D & C panels under construction by AC Spark P lug a r e about 6 weeks behind
schedule due to vendor lead t i m e requi red f o r honeycomb panels.
The b read -
The D Pr C panels
3
for s y s t e m s 1, 2 , 4 , 5 , and 6 are behind schedule.
expected t o be del ivered on schedule ( 1 August 1863) i f a ma te r i a l subst i tut ion of
a luminum and wood fo r honeycomb panelling is allowetl ( for 5A only).
T h e Optical Snbsystem Schedule is shown i n Fig. 1-14.
D & C panels for s y s t e m 5A are
A l l s y s t e m s are con-
s ide red t o be on schedule.
F igure 1-15 shows the del ivery schedule for all Map and Data Viewers . A l l s y s t e m s a re shown as being on schedule.
F igure 1-16 shows the c u r r e n t schedule f o r mid-course guidance s tudies .
Additional s tudies a re being considered and wil l be added t o the cha r t as soon as the
ini t ia l planning is complete.
F igure 1 -17 shows the del ivery schedule for all Raytheon ground support equip-
The f i r s t b readboard computer test s e t is expected t o be del ivered t o MIT/IL ment .
by Raytheon in August 1963.
Raytheon on 28 June 1963.
A computer s imula to r w a s del ivered t o MIT/IL by
Figure 1-18 shows the de l ivery schedule f o r all AC Spark P lug ground support
Th i s schedule is i n accordance with the AC Spark P lug s ta tement of equipment. Work dated 28 Janua ry 1963, with appropr ia te modif icat ions as detailed in the r ecov-
e r y plan authorized by NASA TWX SGC 4-233 dated 11 Apr i l 1963.
T h e breadboard t e s t s e t scheduled for de l ivery t o MIT/IL by AC Spark P lug
on 1 August 1963 is expected t o be about 6 weeks la te .
F igu re 1-19 shows the GSE del ivery schedule f o r Kol l sman Ins t rument Corpo-
This schedule is in accordance with the Kol l sman Statement of Work dated rat ion.
11 Apr i l 1963. with appropr ia te modif icat ions as l i s ted i n the r ecove ry plan authorized
by NASA TWX SGC 4-2'33 dated 11 April 196'1.
In June 1963, MIT/IL, i s sued T D K-75 authorizing Kol l sman t o design and
p r e p a r e f o r manufacture opt ical CSE i t e m s l i s ted below:
I T E M DELIVERY DATE
10 /1 /63 1. P rec i s ion Test F ix tu re 2 . Functional T e s t e r l o / 1 / 63
3 . 5 inch co l l imator 10 /1 /63
10/1 /63 4 . M i r r o r a l ignment f ixture 5. 2-1/2 inch co l l imator 1 O / 1 / 63
6. Short re t roref lec t ing per i scope 10/1 /63
and al ignment equipment
Figure 1-20 shows a PIP del ivery schedule. During May and June, seven PIP'S w e r e acceptance-tested a t Sperry:
PIP No.
1 A P 1 5
1 A P 16
1 A P 17
1 A P l a 1 A P 19
1 A P 20
1 A P 21
Date:
5/20/63 5/24/63
5/24/63 5/28/63
5/31/63
6/14/63
6/18/63
T h e following PIP's have been reserved fo r s y s t e m AGE 5: 1 AP-15, 1 AP-18,
1 AP-19, 1 AP-20, 1 AP-21, 1 AP-22.
F igu re 1-21 shows an IRIG del ivery schedule. During May, two IRIGS w e r e
accepted a t ACSP by NASA:
IRIG No.
1 A-9
1 A-10
Date
5 /8 /63
5/23/63
-
T h e s e a r e the l a s t of 10 ACSP IRIGS received a t MIT/IL. T h e following IRIGS'
a r e r e s e r v e d f o r s y s t e m AGE 5: 1 A-8, 1 A-10, MIT-69.
During the in t e rva l between 1 June and 30 June, MIT/IL, Apollo P ro jec t per- sonnel attended meet ings as shown on Table I.
5
3 2 J
4
I
I 1
4
t t t t
1.
3 d c
V U 1
20:
out
-
0. 0 0
2
r
LY
0
w
a
a
Q: u.
I
rr ,
3 W U
Z O > -
n u n
n u u
Z O > -
L*: E a D U +
Z 0 -
Z 0
000
9
r- 7- 0-
3 w v
10 > - .. .
>VI-
n w n
sa >
a n a
sa a -
R I 1 I I
.
m * 0 (3 U -4 W P 0 I (3
z a W -4
I a
sa * a a a -
n w n
a 2 w
-a z - 3 w v
2 0 > 3U I- -
W J
I- k
li 0 I v)
jooo
_lOOO@
0
1 t W
1 m W
I N W
i 5
0,
f
- o w
20 :
- aa c
1 4 c
o w c
20 :
73 - 73 i - za > an a -
a n a - 5- a
00 CI
ii
7 o w 1
20 : - ou I mw I - I
F .I
W c . -.
. .-
:.. .a: .:.:.:. ....... ....... ....... ....... .e...'. ....... ....
-
- - t ai Y
d 3 Y 0 0 t - 0 -
-
t l
..... t:::?:]
[:;:;FJ ....
-
- - t
a m
a m Q: a!
5
8 0
0 U W
s P a - rn -
LO :
ov c - mw a
1 4 >
aa a
sa o - k w a do
L .rl
o w c
ZO > ov I-
- - - mw a
000
I- In W c 5 z W
m 8 r; U
d, 0 0
U i2
W z u) 000
n - 13
t L
.I
I
t . _- ~
1 4
I t ci 0 ci
. ~ _ _
I I
..... .... ..... .... ..... .... ..... P W I-
-IrL -1 a 5 s -F 3 a 0
-I
2
+ 0 2 3 IL
z W I- 9 c" m 3 rn - *)
-
15
W P 0 I
t I e
000
17
18
P E = I h I ) I
91 % I
2
I
W I
I
R::j ... :::::::i ... ....
...
... .... ... .... ....... ....... ... ~
... ... ... ... ... ...... .... I. ... , .y. ... .... ... .... _..
- I
i
1 -
I
IC ,= : m :>
i9 ! I - s)
-
j I . . . ..... .-.
....
1 @'
. I :. :.I 4 .....
' ' - 1 .... .... .' ..:. . . . ... .... ... .... ... .... ... ....
ll_i 0
:ooo
. w v)
- w J a
- w a
7
i -+- f
t I t t
i l t i W rn
9 W a I---/ z rn W 0
2 t - - f t i - i t t
20
---I-
V U Y
21
A-
+! 1 1-21 I J.
--
.
t t t i I t
-4 - 1
t --I f - .
0, ov t- 1""" ' I 1 2 1 -
2 2
1
' I DDD
-J
0 a
E 0 000 a e t-
I 0
a a W rn
9 W
z rn W 0
a
'3
5 LL
a z I
!E > W 0 0 \ LL a
\ LL a
2 3
d W a,
o w u
20 > - ou c - m w n
sa >
f
k w m
-a z - o w u
20 z
ou t- - - c Y Y
c
g 11 K
fn w g =
I
I
+ t
2 4
000
O W L
20 3 -
an a
s a a - - L W U
-a 2 - O W L
20 >
00 t - I vlwa
s a >
DDD an a
s a a -
L W U
-a 2
O W L
ov I- - v lwa
000
W v)
W J W a z v) W
a
(3
n
0
a3)c
an a- - s a a k w m
-a z o w u
25
26
x t e: I
t t P
w n
r i . . r i I 1 . 1 I
DDD -
...... . . . . . . . . . . . .
...... ...... . . . . . . ... ..... ...... .......
000
W rn
9 W
a z v) W
'2 a
-
z 0 k 5 LL W 0 Y a a
a z z -1
-
i
z 0 t 0 1L a 0 E a a W I a
m V
X __
- I a J
27
W v, (3
z
I I- >
z: 2 8 [r
W -I 3 W I 0 0
U e a t- U I 0 W z 0
W -I
5
b
E: B 1
a
Q o o o o o o o o o o o z w l - t - l - l - t - l - l - l - t - t - l - :I
a: Z
- a - 0
W - I - - 0
' W W
a
I a 0 I-:
- t - 5 - * *
--
c- r--:
+I L
* I I I I I I I I I
29
w u
t 1
t
W v) (3
(3 3 J
Y a v)
0
a
s! a
e I-
U I 0
W z 0
W -I
a
ki
s g
:
- I
J
U
in cc d
4 d r( 1 i:
F4 u . w m
4
m .
> w v
.O >
3 v +
3 w a
I 3 0
€ 4 >
€ 4 u L w m
,a z - 3 w v
2 0 >
V v) 5 0 I-
a U z 0 I-
30
m
E! W
N W a,
t
M N l n N r n - e - - N -
v d
a n
I: i
* * *
J * * *
3 '
32
0
-
0 0 Q
- - - Y t; W I- > z W
0
0
m
? a
- m
-
3 3
TABLE I
Date
3 June
3-4 June
3 - 4 J u n e
4 June
4 - 5 J u n e
5 June
5 June
5-6 June
6 J u n e
6-7 J u n e
10 June
10 June 11 June
11 June 11 June
1 1 - 1 2 June
11-12 June
12 June
12 June
17-18 June
18 June
18 June
18 June
19-20 June
20 June
25 June
25 June
25 June
MEETINGS ATTENDED B Y MIT/IL APOLLO PERSONNEL
P e r i o d 1 June through 30 June 1963
Location
M IT
GAEC
Raytheon MSC
AMR
M a r shall
MSC
KI C
MSC
SRID
M SC San F r a n c i s c o
A m e s MI T
M SC
MSC
GAEC
MSC
MSC
MIT Langley R e s e a r c h Center
MIT
MIT
MSC
MIT
MIT
S&ID
McDonnell Ai rcraf t Corp.
Subject
In-flight T e s t s and F a i l u r e s
LEM Operat ions and Installation
Design Status Review
Apollo S /C Mission T r a j e c t o r i e s Sub -panel
Check -out P a n e l
Crew Safety Sys tems P a n e l Crew Safety Sys tems P a n e l Design Status Review
Navigation and Guidance
Computer and Packaging
Apollo Gyro P r o g r a m Review NASA/Ames Research Center
G&N Simulation Reliabil i ty Meeting GOSS Sys tems Meeting
Crew Safety and Abort P a n e l
Design Review/Operat ions
Apollo Test Sys tems Meeting
GSE Sys tems Meeting
Management Practices
LE M Technica l Conference
I,EM/SCS Interface Meeting
S T U Meeting Document at i on
Simulation Commit tee
G & N Schedule and Test Planning STU/ Design Review
P r o j e c t Mercury Reliabil i ty
Meeting
Coiitrol Review Meeting
34
Date
2 6 J u n e
27 J u n e 27 J u n e
TABLE I (cont'd)
Location MSC MSC
MSC
Subject
Guidance System Meeting # 6
C / M S&C Meeting #16 L E M W / S
3 5
BIBLIOGRAPHY
TECHNICAL PROGRESS REPORTS
No. __
E-1067
E- 1068
E- 1099
E-1116
E-1117
E-1139 E-1140
E-1157
E-1177
E-1199
E- 1236
E-1237
E-1238
E-1302
E-1303
E-1304
E-1305 E-1306
E-1307
E-1308 E-1378
E-1389
Type
Monthly
Monthly
Monthly
Quar t e r l y
Monthly
Monthly Quar t e r ly Monthly
Monthly
Quar t e r ly
Monthly
Monthly
Quar t e r l y
Monthly
Monthly
Quar t e r l y
Monthly
Monthly Q u a r t e r l y
Monthly Mcrnthly
Q u a r t e r l y
Pe r iod Covered
August 11 through September 13, 1961 ( C )
September 1 3 through October 4, 1961 ( C )
October 4 through November 9, 1961 (C) P e r i o d ended December 11, 1961 ( C ) December 11, 1961 through Janua ry 16, 1962 (C)
January 16 through F e b r u a r y 1962 ( C ) P e r i o d ended M a r c h 11, 1962 ( C ) March 11 through Apri l 11, 1962 ( C ) Apr i l 11 through May 1, 1962 ( C )
P e r i o d ended June 11, 1062 ( C ) June 11 through July 1 7 , 1962 ( C ) July 17 through August 21, 1962 ( C )
P e r i o d ended Sep tember 11, 1962 ( C ) September 11 through October 11, 1962 (C) October 11 through November 13, 1962 ( C )
P e r i o d ended December 11, 1962 (C) December 11, 1962 through Janua ry 11, 1963 ( C )
January 11 through F e b r u a r y 11, 1963 ( C )
P e r i o d ended March 31, 1963 ( C ) Month of Apr i l 1963 ( C ) Month of May 1963 ( C )
P e r i o d enfled .June 1963
36
BIBLIOGRAPHY (Cont'd) TECHNICAL REPORTS
R-339
R- 341
R- 342
R- 348
R- 349
R- 353
R- 358
R- 367
R- 368
R- 372
R- 373
R- 376
R- 380
M. B. T r a g e s e r , Guidance and Navigation System Information for Apollo Spacecraf t B idde r s , September 1961 (C)
R. H. Battin, Statistical Optimization fo r Space Flight, September 1961
(Rev. May 1962) (U)
C. S. D r a p e r , W. G. Denhard, and M. B. T r a g e s e r , Development C r i t e r i a
fo r Space Navigation Gyroscopes, October 1961 (U)
E . J . Hall, J. Mil ler , J. Aronson, and A . Lattanzi, Specification f o r P r o -
cu remen t of Apollo Iner t ia l Reference Integrating Gyro, Rev. Aug. 1962 (C)
G. W. Mayo, Guidance and Navigation System Reliability P r o g r a m ,
December 1961 (U)
R. H. Battin and J. S. Mil ler , C i r cumluna r Tra j ec to ry Calculations, Apr i l
1962 (U)
-
R. L. Alonso, A . L. Green , H. E. M a u r e r , and R. E. Oleksiak, A Digital
Control Computer Developmental Model IB, Apr i l 1962 (U)
P. H. Gilinson, J r . , C. R. Dauwalter, and J. A . Scoppettuolo, Mult i range P r e c i s i o n Torque Measuring Devices, July 1962 (U)
G. W. Mayo and E. T. Driscoll , Reliabil i ty Handbook f o r E l e c t r i c a l
Eng inee r s , August 1962 (Rev. October 1062) (U) -
J. H. F l a n d e r s , Velocity Steering Studies for the Apollo Mission, August
1962 (C)
J. M. Dahlen, P. G. Felleman, R. D. Goss, N. E. Sea r s , M. B. T r a g e s e r ,
R. L. White, Guidance and Navigation System f o r Lunar Excur s ion Module,
July 1962 (Rev. August 1962) (C)
R. C u r r y (NASA), 2 Impulse Abort T r a j e c t o r i e s f r o m T r a n s l u n a r Flight,
Oc tobe r 1962 (U)
Development of High Capacity Heat Storage Mate r i a l P h a s e I - Study of Mate r i a l s , J u l y 1962 (U) by Cyro -Therm, Inc.
3 7
R-382
R- 383
R-385
R-386
R-387
R-388
R- 389
R-391
R-393
R-395
R-396
R- 399
R-404
BIBLIOGRAPHY (Cont'd)
TECHNICAL REPORTS (Cont'd)
R. H. Battin, Universal Fo rmulae for Conic Tra j ec to ry Calculations,
Sep tember 1962 (U)
G. W. Mayo, Design Review P r o c e d u r e s , September 1962 (U)
R. C. Hutchinson, Ine r t i a l Orientation of the Moon, October 1962 (U)
___ -. _____ _____
-~
__________
Max P e t e r s e n , E a r t h L imb Definition Photography, MA- 7 M e r c u r y
Flight, Cmdr . Ca rpen te r , (to b e published) (U)
S. J. Madden, Jr . , Orbi ta l Element Var ia t ion f o r a Body in Orbi t
Around the Moon, (to b e published) (U)
~-
______ _.
D. G. Hoag and M. B. T r a g e s e r , Fami l i a r i za t ion Manual (P re l imina ry ) ,
December 1962 (C) -____
G. W. Mayo, Requ i remen t s of and Index to Design Qualification and
Reliability T e s t P r o g r a m , March 1963 (U) ______
D. G. Shepard, The Effect of Re t ro rocke t ____ Exhaust on Visibility dur ing
L u n a r Touch-down, December 1962 (U)
R. L. Alonso, A. L. Hopkins, Jr. and H. Blair-Smith, Logic Desc r ip -
t ion for Apollo Guidance Computer AGC 4, March 1963 (C)
G. W. Mayo and G. Kruszewski , -___ Guidance and Navigation Sys t em
Reliabil i ty Apportionment and ______- Init ial Analys is , F e b r u a r y 196 3 (C)
E. T. Dr isco l l and G. W. Mayo, Apollo Guidance and Navigation
Quality A s s u r a n c e P lan , Apr i l 1963 (C)
W. S. C r o c k e r and I. G. McWilliams, D e s i m and Checking of Index-
ing Volume I1 - G e a r Checking, A p r i l 1963 (U)
N. E. S e a r s , Rada r Rcqu i remen t s for P r i m a r y Guidance and Navigation
Operation, (to be published) (C)
38
BIBLIOGRAPHY ( Cont d)
TECHNICAL REPORTS (Cont'd)
R-405 E. T. Dr isco l l , Quar t e r ly Reliability and Quality Assu rance S ta tus
Report , Apr i l 1963 (U)
R-408 Eldon Hall, Design Concept of the Apollo Guidance Computer , (to be
published) (C)
Eldon Hall, Gene ra l Charac t e r i s t i c s of the Apollo Guidance and Navi-
gation Computer , May 1963 (C) R-410
R-411 D. G. Hoag, Apollo Guidance and Navigation-A P r o b l e m in Man and Machine Integration, Apr i l 1963 (C)
D. J. Lickly, H. R. Morth, B. S. Crawford, &pollo Reent ry Guidance,
July 1963 (U) R-415
39
BIBLIOGRAPHY (Cont ' d)
ENGINEERING REPORTS
E- 1054
E- 1074
E-1077
E- 1078
E - 1091
E- 1092
E- 1097
E-1130
E-1101
E-1103
E- 1104
E - 1106
E-1113
E-1114
E-1118
E-1124
J . Rocchio, Analysis of the ___ P N P and NPN __ Latch Ci rcu i t , September 1961 (U)
D. Shansky, E r a s a b l e F e r r i t e Memory, _MOD 3C Computer , October 1961
(U) _____
R. L. Alonso, J. H. Laning, J r . , and H. Bla i r -Smi th , - P r e l i m i n a r y MOD 3C Computer __ - Pi-ograni, __ November 196 1 (U)
Development _ _ Plan , November 27, l9fil ( to b e r ev i sed ) ( C )
E. J. Hall, Assembly P r o c e d u r e s and Specifications f o r Apollo 25 IRIG,
June 1962 ( C )
J . H. F l andpr s , IMU P ~ . e l i m i n a r y Operat ional Duty Cycle, December 1961
(C)
Work Statement f o r Indus t r ia l S u p p c , J anua ry 1962 (C) Addendum, F e b -
r u a r y 1962 (C) _ _ _ _ - ~
M. Sappupo, Work s t a t emen t f o r P I P MOD D, December 15, 1961 ( C )
E. J . Hall, Work Statement f o r Apollo 2 5 IRIG, December 15, 1961 (C)
E. J . Hall, - ~ - Assembly P r o c e d u r e s and Specifications f o r 2 5 IR MARK 45
MOD 2, December 15, 1961 ( C )
M. Sappupo, __________ P r e l i m i n a r y Assembly and Test Manual 16 PIP MOD D,
J a n u a r y 19G2 ( C )
P. G. Fel leman, - Analysis of Guidance Techniques for Achieving Orb i t a l
Rendezvous, J anua ry 1962 (U)
Sys t em Identification Data List, (SIDL), ( i s sued August 20, 1062) ( to be r e -
vised and supplemented monthly)
J. E. Levy, G lossa ry of T e r m s and Symbols, Apr i l 1962, (Rev. Ju ly 1962)
(C)
R. A . Scholten and P . J . Philliou, - Investigations of Midcourse Maneuver
F u e l Requirements , March 1962 ( C )
J. S. Mi l l e r and J . J. Deyst, P r e l i m i n a r y Study of A b o r t s from C i r c u m - luna r T r a j e c t o r i e s , M a r c h 1962 (U) _-__-____-
40
BIB LIOGRAPMY (Cont ' d)
ENGINEERING REPORTS (Cont 'd)
E-1125
E-1126
E-1130
E-1131
E-1134
E-1142
E- 1144
E-1158
E-1161
E- 1164
E - 1167
E-1172
E-1173
E-1179
E- 1186
E-1195
E-1196
E-1203
R. L. Alonso, P r e l i m i n a r y Resolver Angle Measuremen t s , F e b r u a r y 1962
(U)
A. L. Hopkins, J r . , AGC MOD 3C Computer C i rcu i t s -Genera l , F e b r u a r y
1962 (U)
J . E. Levy, Maintenance Plan, March 1962 (U)
J. S. Mi l l e r and R. H. Battin, P r e l i m i n a r y Summary of Data f o r a Variety
of C i rcumluna r T r a j e c t o r i e s , Feb rua ry 1962 (U)
A . C. Hardy, Pho tomet r i c Units in the MKS System, March 1962 (U)
J . E . Levy, Weight and Balance Report , 15 March 1962, (Revised Ju ly 1962) ( to b e r ev i sed monthly) (C)
J . E. Levy, Apollo Guidance Navigation In t e r f aces ( to be published) (C)
D. Shansky, E r a s a b l e S to re MOD 3C, Ju ly 1962 (U)
I. Halzel, Technical Direct ive P r o c e d u r e s f o r Apollo G & N Sys tem P a r t i c -
ipating Contractors, . May 1962 (U)
F. D. Grant , The Relationship between IMU Drift Misal ignments and T a r g e t
E r r o r s , May 196'2 ( C )
Drawing Standards, 15 J u n e 1 9 6 2 (U)
A. C. Hardy, The Visibil i ty of S ta r s , June 1962 (U)
R. M. Jansson, The Heat T r a n s f e r P r o p e r t i e s of S t ruc tu ra l E lemen t s f o r
Space Environment, J u n e 1962 (U)
R. G. Scott, Rope C o r e T e s t e r , Ju ly 1962 (C)
Technical Data Re lease P rocedures , August 1962 (U)
--
-
-_
-
I
N. E. Sea r s , E a r t h Orb i t a l Rendezvous, May 1962 (C)
M. W. Johnston, - Analysis of Two Lunar Landing Techniques Providing
Di rec t Landing Site Visibil i ty P r i o r t o Touchdown, July 1962 (U)
G. A. Davidson and H. H. Seward, Cal ibrat ion Techniques f o r P r e c i s i o n
Rotary Components, August 1 9 6 2 (U)
41
BIBLIOGRAPHY (Cont 'd)
ENGINEERING REPORTS (Cont 'd)
E-1212 ' F. D. Grant , Error Data S u m m a r i e s for Var ious Tra j ec to r i e s , (Prelim-
inary) , Sep tember 1962 ( C )
T. C. Tay lo r , T h e r m a l Models for High Density Computer Ci rcu i t
S t ruc tu re , Sep tember 1962 (U) - _____._
E-1215
E-1230 J. E . Mi l l e r and J . H. F lande r s , ____- Comprehensive Alignment Test for IMU,
(to b e published) (C)
E-1233 T. C. Taylor , Technique of C i rcu i t Fabricat ion with State-of-the-Art
Weldable Multi layer Boards, October 1962 ([J)
E-1256 J. W. Hursh, Apollo Midcourse Guidance, November 1962 (C)
E-1257 L. J . La reau , A tmospher i c -_ Refraction as a Means of Horizon Determination, -
December 1962 ( U )
E- 1260 P. K. Bryant, P r o c e d u r e s of the Apollo Management, ( to be published) ( C )
E-1261 G. M. Levine, Application of Midcourse - Guidance Techniques t o Orbi t
Determinat ion, December 1962 ( U )
E-1278
E- 1285
E-1287
E-1288
E-1293
E-1297
E-1313
E-1322
G. Gi lber t , MIT Space Implementation, In t e r im Report , J a n u a r y 1963 (U)
A. C . Hardy, Some Luminance _______~ Values for Sun, Ea r th , and Moon, J anua ry
1963 ( C )
J. M. Dahlen and J . H. Long, Back-up ._ Thrus t Vec to r Control, F e b r u a r y
1963 (C)
F. D. Grant , Alignment E r r o r s of t he IMU Stable Member, F e b r u a r y 1963
(C)
R. Boyd, AGE Fie ld Operat ions - P r o g r a m Plan, A p r i l 1963 (Prel iminary)(U)
J. H. F l a n d e r s , Ine r t i a l Subsystem (ISS) Cal ibra t ion Tests, (Pre- l imina ry ) June 1963 (U)
T. C. Taylor , T h e r m a l Grounding - Analysis f o r Ci rcu i t S t ruc tu res , (to be
published) (U)
G. W. Mayo, Apollo G & N - F a i l u r e Reporting and Cor rec t ive Action P lan ,
Apr i l 1963 (U)
42
BIBLIOGRAPHY (Cont'd)
ENGINEERING REPORTS (Cont'd)
E-1342
E-1343
E-1344
E-1350
E-1353
E-1359
E-1363
E-1374
E-1381
E-1385
E-1386
Apollo Guidance and Navigation Equipment Fami l ia r iza t ion Manual,
(to b e published) (C )
G. Oberbeck, T e r n a r y Pulse Torquing, May 1963 (U)
D. G. Hoag, Considerat ion of Apollo IMU Gimbal Lock, Apr i l 1963 (U)
W . Br iggs , S ta t i s t ica l Decision Theory for Logis t ics Planning, May 1963 (U)
E. Copps, D. A. Koso, D. Nordvedt, and M . B. T r a g e s e r , E a r t h Pa rk ing Orbit; Guidance and Navigation Measurements , (P re l imina ry )
(to be published) (U)
J. Dahlen, T. Heinshe imer , J. Suomala, Flight Test P lan - Apollo
G & N System AGE 5, May 1963 (C)
T. Heinshe imer , Status of Apollo Flight Safety System Design and
Development, ( to b e published) (U)
J. Sciegienny, Propagat ion of t he Altitude and Altitude Rate E r r o r s
during the Suborbital Flight, ( to b e published) (U)
R. Boyd, Data Analysis and Disseminat ion Instruction, ( to be pub-
l i shed) (U)
( P r o f . ) Hardy, Visibility Data and the Use of Optical Aids, (to be
published) (U)
S. Smith, Report on C l e a r Resins, ( to be published) (U)
43
T-351
T-352
' BIBLIOGRAPHY (Cont I d)
THESIS REPORTS
M. A. Lanman, Analysis of a Posi t ion Control Servo Incorporat ing
Quantized Feedback, May 1963 (U) . - __ .-
- R. L. Fortenbaugh, Descr ipt ion and Analysis of the Apollo Space
Sextant Simulator , May 1963 (U)
44
E- 1389
DISTRIBUTION LIST
Internal
R. Alonso
J . Arnow (Lincoln)
R. Battin
W. Bean
E. Be rk
P. Bowditch
A. Boyce
R. Boyd
P. Bryant
R. B y e r s
G. C h e r r y
E. Copps
W. Crocke r
G. Cushman
.J. Dahlen
M. Drougas
E. Duggan J. Dunbar
K. Dunipace (MIT/AMR)
R. Euvra rd
P. Fe l leman
S. Fel ix (MIT/S R ID)
J . F l ande r s
J. F leming
L. Gediman
F. Grant
Eldon Hall
I. Halzel
TI. Hanley
W. Heintz
E. Hickey D. Hoag
A . Ilopkins
F. Houston M. Johnston
B. Katz
A. Koso
M. K r a m e r
W. Kupfer
A. Laa ts
D. Ladd T. Lawton
D. Lickly
R. Magee
G. Mayo J. McNeil
R. McKern
J a m e s Miller
John Miller
J. Nevins
G. Nielson
J. Nugent
E . Olsson
C. P a r k e r
J. Pot ter K. Samuelian
P. Sarmanian
R. Scholten
J. Sciegienny
N. S e a r s
D. Shansky
T. Shuck W. S tamer i s
E. Stirl ing
R. The r r i en
W. Toth M. T r a g e s e r
R. Weatherbee
L. Wilk R. Woodbury
W. Wrigley Apollo L i b r a r y (2)
MIT/IL L i b r a r y (6)
E x t e r n a l
(ref. APCAN; 2 Ju ly 1963)
P. Ebersole (NASA /MSC)
W. Rhine (NASA/RASPO)
S. Gregorek (NAA S & ID/MIT) AC Spark P l u g
Kollsman
Raytheon
WESCO
Capt. W. Delaney (AFSC/MIT)
NAA R A S P 0
CAPE:
HDQ:
AMES:
LEWIS:
FRC:
JPL:
LRC:
GSFC:
National Aeronaut ics and Space Adminis t ra t ion Resident Apollo Space c r a f t P r o j e c t Officer North Amer ican , Inc. Space and Information Systems Division 12214 Lakewood Boulevard Downey, Cal i fornia
National Aeronaut ics and Space Adminis t ra t ion Atlant ic Miss i le Range Operat ions Port Canaveral , Flor ida Attn: Mr . B. P. Brown
NASA Headquar te rs 1520 H Street Washington, D. C. Attn: Mr . G. M. Low, MD(P)
National Aeronaut ics and Space Adminis t ra t ion A m e s R e s e a r c h Center Moffett Field, California Attn: Mr . Matthews National Aeronaut ics and Space Adminis t ra t ion Lewis R e s e a r c h Center Cleveland, Ohio
National Aeronaut ics and Space Adminis t ra t ion Flight R e s e a r c h Center Edwards AFB, California
National Aeronaut ics and Space Adminis t ra t ion Jet Propuls ion Labora tory Pasadena , ,California Attn: Mr. H.R. Lawrence
National Aeronaut ics and Space Adminis t ra t ion Langley R e s e a r c h Center Langley AFB, Virginia Attn: Mr . A. T. Mattson National Aeronaut ics and Space Adminis t ra t ion Goddard Space Flight C e n t e r Greenbel t , Maryland
(3)
NAA: North Amcit.ic:an Aviation, Inc. Space and 1nfoI.mntion Sys t ems 1)ivision 1 2 2 1 4 1,:lltewor)tl I3oUlev:lI-d 1 iiwne y , C: :I li f I) rni:] Attn: Mi.. 11. 13e1.i-y
G A IK: National A e 1-onaut i c s rind Spac,c Administr-ntion (1) I < A SPO: l iesident A p o l l o Spacecraf t P r o j c c t O f i '' l C < ? 1.
Grumm an A i rc r n i't I<ngincc: r ing <: orpornt i on Bethpage, L.I. , N e w Yurk Attn: M r . Jack Small
Pos t Ol'f'ice I> i .awer U White Santls Miss i le Iiangc White Sands, N e w Mexico
Manned Spacer i.aTt C e n l c ~ . Apollo Ilocumerit Conti-01. Group (SDG) I lous ton I , Tcxas
WSMK: N xti onal Ae r onuutic s and Spare A tfminist rnt i on (2)
M SC : National Aer.on;iutic:s rii i t l Sparc Administration (60 )
top related