NRO ?PROVED FOR 

RELEASE 1 JULY 2015 

V. HANDLE VIA BYET/TAN 

CONTROL SYSTEM ONLY 

PROGRAM SCHEDUTF. 

STATUS 

10 JUNE 969 

SAFSL-1B 

PROGRAM COTITROL 

DIRECTORATE 

4 

HANDLE' VIA BYEl'an 

CONTROL SY.E3TENT crsp_.( 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

• 

HANDLE VIA BYEMAN 

CONTROL SYSTEM ONLY, 

CONTENT 

1. MDAC-WD 

2. GE 

3. EK 

4. MDAC-ED 

5. T-IIIM 

6. HAVELTON STANDARD 

7. CHRONOLOGY OF MAJOR EVENTS 

8. MOL LAUNCH SCHEDULES 

'HANDLE IPA 731,17,7,7,7-1 

CONTROL SYSTE,1 C.NLYa 
NRO APPROVED FOR 

RELEASE 1 'JULY 2015 

CONTRACTOR: VeDONNELL DOUGLAS-WESTERN DIVISION 

STATUS OF 

10 June 1969 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 SECRET awl 

MDAC-WD PROGRAM CONUOL 

Performance 

Overall performance of the tasks for WBS Areas 8101, 8103, and 

8104 was satisfactory. These tasks include the effort expended for 

both MOL Program Integration (MTT) and the MDAC-WD associate contractor 

activity. SAFSL Exhibits 21002 and 31002, "Schedule Control System" 

provided guidance for these tasks. The MPI effort averaged approximately 

12 men and the associate contractor manpower averaged approximately 

24 men in support of the PERT/Time and schedules activities. 

CDRL Submittals 

The data items listed below were submitted by MDAC-ND from the 

date indicated for the first submission through 10 June 1969. All 

submittals were acceptable. 

WBS 8101 

Sequence No. 

44 

Description 

Submission 

Cycle 

First 

Submission 

Assoc. Part of MOL 10 Oct 66 

Schedule (Internal Delivery 

from Assoc. a)mPI) 

Monthly 

Sequence No. 

WBS 8103 

Submission 

Cycle 

First 

Description Submission 

20 Red Flag Rpt As Req None 

21 Problem Analysis Rpt Bi-wkly 22 Oct 66 

24 Detail PERT Act. Rpt Qrtly, as req 1st PERT cycle 

25 Summary PERT Act. Rpt Bi-wkly 21 Oct 66 

27 Sinnmary PERT Event Rpt Bi-wkly 21 Oct 66 

34 Detail PERT Network Qrtly, as req 21 Sep 66 

35 Summary PERT Net7ork Bi -wkly 21 Oct 66 

38 

42 

Topical Graphics/Shredouts. 

Summary Event Dictionary 

Submit 4 times 

Bi-wkly 

None 

4 Nov 66 

45 Simulation Rpt Annly None 

WBS 8104 

Submission First 

Sequence No. Description Cycle Submision 

22 Integ Problem Anal Rpt Bi-wkly 28 Oct 65 

26 Integ Summary PERT Act Rpt Bi-vkly 26 Oct 66 

srcp T nrxrx1 

g' • 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

WBS 8104 (Cont) 

Sequence No. Description 

Submission 

Cycle 

First 

Submission 

28 Integ Sumnry PERT Event Rpt Bi-wkly . 26 Oct 66 

29 AFPITI PERT Event Rpt Bi-wkly 26 Oct 66 

36 AFPMN PERT Network Bi-wkly 26 Oct 66 

37 EDAe-ED, GA EK PERT Networks Bi-wkly 16 Jan 67 

(Converted from Schedules) 

43 MOL Sys, Integ Schedule (Overt)Mthly 10 Oct 66 

44 MOL Syc. Integ Schedule Mthly 10 Oct 66 

46 Simulation Rpt Annly As Req (Twice) 

47 Integ Interface List Bi-wkly 16 Jan 67 

Products on non-Dorian DD 1423: 

WBS 8101 

Submission First 

Sequence No. Description Cycle Submission 

B226 Master Schedule Monthly It Nov 68 

VW 8103 

Submission First 

Sequence No. Description Cycle Submission 

B214 Red Flag Rpt As Req None 

B215 AFSC Form 30 'Pert Input' Bi-wkly 21 Sep 66 

- (Computer Card Deck) 

B228 PERT Networks (Detail) As Req 23 Sep 66 

B229 Topical Graphics'Shredouts As Req None Required 

2 

. 
NRO APPROVED FOR 

RELEASE 1 'JULY 2015 

01711 11 

mm■i‘-■j2:10..":". .1]r 1":24 

- STATUS OF MDAC-ND EFFORT AS OF 10 JUNE 1969 

I. AVE DESIGN FABRICATION AND TEST 

1. Design Engineering - 35% (Much of the Design effort is further 

defined on subsequent items) 35% Based on Design effort required to complete 

Program and 70% based on Design effort required to reevaluate Program. 

2. LM Development Fixture - 50% assembly had been completed and 

development of wiring and piping was started - 15%. 

3. MM FWD and AFT Sections - 15% shipments had been on schedule, 

however, rework to the "Fburbh Mode" specification was necessary on two 

delivered articles. 

4. LM Substitute Structures and Interface Hardware - 45% these 

items have been on schedule. 

5. EDCTU Assembly and Installation - 65% "Ft wer On" has been predicted 

as being 13 weeks late. Testing had not started at the System level. 

6. AVE - 5% with some subassembly started on Flight-2. Tooling 

and manufacturing accounts for most of this activity. 

7. LM and MM Static Test - 30% at the subcomponent levels and 

support to other A/C. 

8. Im and MM Dynamic Test - 8% 

9. AVE Development Tests - 35% subsystem testing only. 

10. AVE Qualification Tests - 10% component levels and sUbcontractor 

testing. 

11. EC/LS - 15% Facilities and planning; very little AVE Assembly 

12. MSK Effort - 48% 

II. AGE 

1. AGE - Huntington Beach - 20% 

44,41, 71/1 

• 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

2. AGE - SACTO - 15% This item has been behind schedule; as much 

as 4 to 5 months. 

3. AGE-VAFB - 20% 

III. SIMULATION AND TRAINING 

1. Mission Simulator - 70% This item was in final installation and 

checkout at Huntington Beach. Training was in a very preliminary phase. 

IV. SOPIWARE 

1. Software - 20% Delivered MOL TOL Compiler. 

V. SITE ACTIVATION 

1. Site Activation (VAFB) - 1% 

' 
n B B 

a 

0 

g 

Z 1666 SY 1.1161,071 77 73 14 76 76 

B B n 

a B in 

B 

N© a Eil B B 

n B II 13 B

B B 

1TEG, GETS C10, AVE/AGE IF DEV 

2930 31132 33 34 35$6 31 34 39 401 

13 13 13 1211 13 13 53 

5313 

0 MONTHS FROM EDP ATP 

0 
Lc) 7; 

O N 

LL 

>- 

o

LL1 D > —3 

a I-U 0_ Up 

< < O -J 

LL1 

Z 

a 

r, 

. . 

. . 

MDACAVD . 

MASTER SUMMARY SCHEDULE COMPREHENSIVE SUMMARY (CONT) 

FISCALYEAR FY68 I FY69 1 FY70 1- FY71 1 FY72 1 FY73 I 

CALENDAR YEAR 1968 7 1969 1970 

_ 

1971 1972 1973 

, 

MONTHSMAMJ JAS ONDV FMA MJJAS ON O1FM AMJJ AN OND/ FMA MIJ ASO NIOJ EMAMJI AS ION D V F57,A MII A 

- 

4i MONTHS FROM EDP ATP 19120 21 72123 24 75262/28203031 32 13 34135 15 317 38304041 4214346 65 66 47 46.61150 51 52 53 54 55 56 57 SO 59 60 61 6216364 66 66 67 5660 70 71 77 73174 75 76 /V 71 795081 62 8384 

s--•(:) 

. 

Fa 'T 

— ,; 

s 

<3 .3.' 3 

2.0 

tt--.0 

,....i.,• 

2•(3-1.7<tJ - .(3 

--ks 

2 

--is 

OIL 30 APRIL 1066 

TOO 

TOD 4 

II ,4 A 6 a • 

' 29 

. 6 

4 161 77 

6 9 6I. 

ttr.o 

DEVELOPMENT 

FLIGHT 22 

Sr TOTAL EFFORT 

a 

r.• 7:- 1- i 

A, V---- 

V T. 

..T 

R 

g 

V 

jr..% 

g 

'T 

L 

2 

1 

..:___ 

2 -r -g- 

—, 

;,. 

..— g 

X 

,..— R -r 

- - Fr 

R -g- 

-1- 

X X 1--- a -..- R r-- a 

R 

U 

ei 0 0 LZ' p4.7 . 14 et) 

. er le , f, tt' r - ., < › 01 

■- 

E - cr 0 - ' 0 2 - g ii t,- - E - r, ts fe NW f, 1 >, :5 . 1 t5 g 

i 

8 

., 

O 

.t. 8 2.3 E 5.3 e 5 ,J ,.2 il: F. a a ., z a 2 > .J o a 

C 

.., 

.1> 

• 

MONTHS FROM EOP ATP 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

1 HANDLE VIN BlitMAN 

CONTROC SYSTEM ONLY 

CONTRACTOR: GENERAL ELECTRIC 

STATUS AS OF 

10 June 1969 

vmNprt Y525! - BYVIVI 

"CONTROC. -SYSI-171 
NRO APPROVED FOR 

RELEASE 1 :JULY 2015 

SOW PARA. 19.0 (Pa. 61) 

TITLE: Management 

PERCENT COMPLETE: 35% CONFIDENCE: ± 5% 

BRIEF DESCRIPTION: 

19.1 Program Management 

19.1.1 Planning, Scheduling, Status Report 35% 

19.1.2 Schedule Control System 40% 

19.1.3 Cost Planning Control System 4056 

19.1.4 EMC Control Program 35% Lupfer 

19.1.5 Cost Proposal for Flt 6 & 7 100% 

19.1.6 Transition Bldg 8310 80% Campbell 

19.2 Configuration Management 30% Barry 

19.3 System Effectiveness Management 30% 

19.4 Contract & Management Systems 35% Edwards 

19.5 Travel and Living N/A 

19.6 Subcontract Management 35% Edwards 

.As management of program is required throughout the program, this 

task completion should be proportional to the degree- of completion 

of the segment at the date of termination. (Adjustment was made for 

the fact that reduced management is required as program nears completion.) 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

SOW Par. No. 19.0 Para. No. 19.1.1 

TITLE: Program Management - Program Planning, Scheduling, Monitoring, 

Reporting 

% Complete 35% 

The contractor's basic program planning, control, and reporting system has 

been in existence for 22 years and fully operational for 2 years. There 

are 3 major program years remaining which would indicate that the contractor 

was 40% complete because this is a Level of Effort type activity. However, 

the contractor would still be required to prepare detail schedules for 

flights 3-5, which brings the % complete down to 35%. 

Confidence Level - High 

SOW Par. No. 19.0 Para. No. 19.1.2 

TITLE: Program Management - Schedule Control System 

% Complete 40% 

The contractor has established the Master Schedule and all remaining effort 

will be monthly updates and delivery. The other major effort in this 

task is PERT Time. The PERT Computer Program has been written. However, 

a great deal of work remains over the next three years: The contractor 

must provide more detailed logic for the current fiscal year and then 

detail the program as it progresses. Two of the five big years have passed 

and this is a level of effort type activity and for this reason plus the 

preceding reason, this effort is felt to be 40% complete. 

Confidence Level - High 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

SOW Par. No. 19.0 Para. No. 19.1.3 

TITLE: Program Management - Cost Planning Control System 

% Complete 40% 

Although the contractor has completed the design and documentation of 

his Cost Planning and Control System and has demonstrated his system, 

there still remains a continuing level of effort activity during the 

next three years. The contractor will still have to crank in budgets 

and milestones and discipline the system. 

Confidence Level - High 
NRO.APPROVED FOR 

RELEASE 1 JULY 2015 

STATUS OF G.E. EFFORT AS OF 10 JUNE 1969 

I. AVE DESIGN FABRICATION AND TEST 

1. Engineering Model 103 (MM) - The delivery of this model is 100% 

complete. Minor refurbishing was in process prior to shipment. 

2. Engineering Model 103L (111) - The delivery of this model is 100% 

complete. Minor refurbishing was in process prior to shipment. 

3. GD -2 (Refurb. 102L & Ship) - This shipment had been completed. 

4. Breadboard Testing (BB-1) - This testing was virtually complete. 

5. Component Dev Model Procurement & Fabrication - 60% of the procurement and fabrication of the development components had been completed. 

6. Component Development Model Test (DC-1) - 40% of the test activity 

has been completed. 

7. Subsystem Development Model Procurement & Fabrication (DSS-1) - 15% 

of the procurement and fabrication for the DSS-1 test had been completed. 

8. Subsystem Development Model Test (DSS-1) - 15 - 20% of the DSS-1 

testing had been completed. 

9. GE-AVE Structure Test Vehicle (113D) - The delivery of this test 

vehicle is 100% complete. The contractor has completed approximately 40% 

of the testing. 

10. GE-AVE Thermal Test Vehicle (113T) - Plans for 113T testing had 

been completed and the test vehicle was ready. Testing had not started. 

11. GE-AVE System Development Test Vehicle (114) - The test vehicle 

had not been delivered nor had testing begun. 

12. qualification Test Vehicle (115) - The test vehicle had not been 

delivered nor had testing begun. 

13. MCC to MDAC-WD from GE (Ship) - Not scheduled until FY 71. 

II. AGE 

It is estimated that 42.4% of the total AGE system was completed by 

the contractor at the time of termination. 

1. MOL CITE - 50% of this AGE system was completed by the contractor. 

No deliveries had been made. 

2. MMTE (CITE) - 12% of this AGE system was completed by the contractor. 

No deliveries had been made. 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

SIMULATION AND TRAINING 

1. NDS (106) - Hardware design and fabrication was essentially 

complete. Checkout was in process for Phase Zero configuration, but had 

not yet been completed. The contractor was approximately four (4) months 

behind FY 69 schedule. In summary, about 75% of the hardware design and 

fabrication and checkout system had been completed. 

2. IviSE (111) - About 10% of the design, fabrication, and checkout 

of the NNSE had been completed. 

IV. :SOFTWARE DEVELOPMENT 

1. CEI - CDR - Only the 805 CDR had been completed by 10 June 1969. 

2. CEI-FACI - Not scheduled in FY 69. 
'44 

0 

0■4 

vJ 

• r4 w

0 I 

V 

ti) 

U 

to 

cd 

cr• >4 

0 Figure 2-3. 

.10% 3

rn

r1 

cw 

0 

3 

0.o C•1 

>•• 0 _1 

LL 

> 

o 

cc 0_ w ) 

o_ 

a - w o 

z ce 

MMSSMOL FY 69 BASELINE SCHEDULE REVISION 1 

FY69 j FY70 FY7 1 FY72 F1'73 FY74 

I r [A 1411A151.1 , 1 

al ..1. 

al 

cc, 

tv CD 

to 

cn 1.- 

--go 

, 

co 

cro 

a3 

S 

cn 

, 

, 

r... 1.. 

ti 

N 

—. 2 

b 

0 

El 

1211 

.... 

C .... 1 

,..... 

0 P2 .---- _ x r.... 

. g rA 

.... 

co 4 ,,, 

- 0 

..- 0 

1212 

DEN' M A 

. . 

,.

.._.,,,, 

0 

. 

1 

A, 

e0 ..., . - N Zn 

,-..-.- . 

.. . 

.- 

F l 

rs Eil

0 

2 o ;;-, 

0 

0 

.-.-....- At 

W ey 

<Ir ., 

3 . 

CV O

. 

El 

N. 

. 

G 

0 1'. 

.." 

2 3 25i:S.n.13 i!Zp.3:!401051 

FISCALYEAR 

CALENDAR YEAR 

MONTHS 

MONTHS FROM EDP ATP 

[MCA. FL IGHT DATES 

18 AVE DES IGN FABR ICATION & TEST 

1. 

Hardeiare Des ign Releases 

2. 

Des ign Rev iew & Buyoffs 

' 3. Engineering Model 103 IMMI 

4. 

Engineering Model 1031 (IM) -/ 

5. 

GD 2 MDF for DACO Refurb. 102L ■I 

ra. 

. — 

.0 

4,1 

c.3 

6. 

Breadboa rd Tes ting (BB-11 ' 

7. 

Conpn OevModel Proc,;&Fab(1:1C-11 

8. 

Compri DevModel Test( DC -1) 

9. 

SubsysDev Model Proc& Fab ( DSS-1I 

10. 

SubsysDev Model Tes t (DSS-11 

[ 11. Compon Qual Model Proc& Fab 

(..) 

12. Compon Qua l Model Tes t (QC-1) 

'13. GE-AVE Struc t Test Veh (11301 t/

. 

14. GE-AVE T herma l Tes t Veh 11131) 

15. 

GE-AVE SysDevTes t Veh (114) %/ 

16. 

GE-AVE SysPPAC Devel. (114E) t' 

17. 

Qua l Tes t Vehicle (115) u 

18. 

GE-AVE forFl ight 2 (116) 

19. 

GD 6 LMQ11/ Equip. 

20. 

GE-AVE(MA) for Flight 3 (118) 

21. 

GE-AVE (MA) for Flight 4 (119) 

MONTHS FROM EDP ATP ' 
VA 4-1 Y i3 

j 

3 

I 

CC 

0 W 9 c

0 _ >- j W 

> —3 

0 LC W 

ci) 

< 

0 

w 

z 

MMSS MOL FY 69 BASELINE SCHEDULEREVI SION 1 

FY69 FY70 1 FY71 I FY72 FY73 FY74 I 

.....■ 

ti 

. 

2 

. 

". 

P,- 

..6 

a, 

. . . 

FI141.4 1, 1 

/8.75;80181182;8384185 

VI' 

a/1 

43 

,.._ _.. f...._ 

} t; •;,-' 

N 

1 

-0; 

-'- 

. Ifi 

....-.. 

t* , 

6,110 A 

T 114EL116d( :'A 

e8Q115An5 /219 

A"8 

6■ 191 

6:1861■ 15A".6 

 I 

DAC 

40013 

• 

2 7.., 

0 

,e 

0 sr 

I. I. 

x sr *a sr sr• 

sr 

... V- 

..7, 7

■ -. .;!F IM; A i M IJ IJiltI SI O iN iD 23,24.2!• 2 i.:-:2B12i%17.17.2;33P4135 3601138139 4(: 

FI SCAL YEAR 

CAL EN DAR YEAR 

MONTHS_ • 

MONTHS FROM EDP ATP 

. 

_ 

'***4 

0 

(NI 

4.) 

a) 

41) 

JJ 

0 

C4 

V 

5 

U) 

.-4 

cel 

sx) 

0 
NRdAPPROVED FOR 

RELEASE 1 JULY 2015 

Haivoz.zETEZZIAr corvrizot: sYsreAr 

stiAlCa 

CONTRACTOR: EASTMAN KODAK 

STATUS AS OF 

10 June 1969 

E• rf" v.,' '41" 

CONTROO,YSf "... 
NROAPPROVED FOR 

RELEASE 1 JULY 2015 DORIAP1 

STATUS OF E.K. AS OF 10 JUNE 1969 

L. SDM-1 The lens assembly was completed in May 1969. The Mission 

Module Aft Section (D2-1) and handling equipment GE-411 

GE-43, GE-47, D2-12A, DE-15B, DE-16A and DE-40A were 

received in May 1969. SDM-1 was 90% complete. 

2. SDM-2 The first lens assembly for SDM-2 was completed in August 1968. 

A decision was made to replace the Camera Optical Assembly 

and the first lens assembly was disassembled. The second build 

up of the lens assembly had not started and the SDM-2 was 

45% completed. 

3. THERMAL MODEL 

The thermal testing of the lens assembly started in January 

1969. The thermal model was 60% complete. 

4. OPTICAL ASSEMBLY TEST 

The subassemblies of the lens assembly were being worked 

but none were completed. The Optical Assembly Test was 

35% complete. 

5. ENGINEERING MODEL 

The lens assembly had been dynamically tested and the subassemblies had been inspected for any degradation. None 

of the subassemblies were completely rebuilt or installed. 

The Engineering Model was 45% complete. 

6. QUALIFICATION MODEL 

Work had just begun on the subassemblies of the Qualification 

Model with less than 3% of the work being done. 

7. FLIGHT MODELS 

No work had started on the flight models. 

PIM 
SUMMA RY SCHEDULE 

X 67 '69 1 '70 7 Il ,7a 1 '73 I0, 

.... 

l. 

I 

• 

X H 

••• 

•.-....,A 

4-1 A ve q=1 I 

- t 1.4... 

Ell 

.... 

1.• 

ci 4.- 

0 

< t 

I-I e..., 

111 fli < 

i-, 

. - 

t••• 

lT 

r:2 4., n 1 

c. 

III 7 

,., 

..„, 

• 

(-I 

..../.=. II 

t-.1 

= 

CZ ...:". 

........ 

= p 

.... S i 

ca _f 

-....... 

O. 

Q, 

- 

Cli 

0 

.7.: 

a' 

. 

,.., r--- 

*...L.. 

, 

..c r 

h--, - 

..... 0:=1 

7.-_-• ,,,, 

II 

I 

I 

i 

141411 Ilb, -■ 

!II% 

1167% 

■ 

GI ' 

0 '...; -1 

■ 

411 ., 11

In ,..4 

r....- 

tiLl" 

an 

......"

r-I 

1-. '--- 

O. 

- 

r0 '-'' 

---.: 

r4 

0 rz. 

v*, .•-• 

I-) 52 0iji 

c., ..... 

-c c0 

NZ 

• 

U, 4' 

FISCAL YEAR 

ICALEN DA R YEAR 

kri 

1 I-- 

Z 

0 

Z 

a. 1-* 

< 

a. 

a 

Lu 

1 

Z 

01, 

43 N 

8 

E 

fX 

(.6 113 

CI 

< 

2 

i-I -4 1

N g 

01 0 

z 1'o 1

2 8 t.-. 

. 

. 1-1 2 ul Q IA 

rl Q z c."

0 1-1 173 t 

c2, 2 

1-4 

H CV V\ 4.: .4a: 

0 til ti 

0 0 2 

= x x 

0 0 0 H 

MNNM 

1 

4 

0 

• 29 A. 

0 I-4 

4.- 4: 

Ki 

0 X 

0 H 

trN 

MASTER SUMARYSCHEDULE 

U) 

4.) a) 0 E-• 

rig 

E -4C

. 

LI 

r-1 N Crl v\ 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

CONTRACTOR: MeDONITELL DOUGLAS-EASTERN DIVISION 

STATUS AS OF 

10 June 1969 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

STATUS OF MDAC-ED AS OF 10 JUNE 1969 

I. ENGINEERING' 

MAC-ED was 69A complete with the drawing releases and had completed 

the CDR in the AVE and AGE. 

II. GROUND TEST PROGRAM 

The Electronic System Test was 91% complete, Structural Test was 

54% complete and the thermal vacuum test was not started. 

III. AGE SUMMARY 

1. AGE at St Louis - The AGE manufacturing assembly and checkout 

at St Louis was approximately 50% complete. 

2. AGE at VAFB - The fabrication and assembly of AGE.at VAFB was 

5% complete. The GBPS was 75% manufactured but was suffering a four-month 

delay because of a lack of interface definition with STC. 

IV. MANUFACTURING AND INTEGRATION 

1. Flight Hardware - The manufacturing and assembly of flight hardware was to begin 1 July 1969 with AVE-1 GBQ. Subsystem components for 

GBQ had been manufactured and were ready for assembly. No other flight 

hardware had been produced as of 10 June 1969. 

2. Test Hardware - Approximately 80% of all test hardware was completed 

as of 10 June 1909. Electronic test unit, 100%; Static Adapter, 100%; Re-Entry 

Vehicles, 100%; Boilerplate-1, 100%; Boilerplate-2, Thermal Vacuum Test 

Article, 30%; and Flotation Egress Trainer, 10%. 

V. FACILITY ACTIVATION 

The Engineering and Operations Building at VAFB was complete and 20% 

outfitted. AGE and General Support Facility was completed and was 5% outfitted. 

Work in support of the Launch Control Center and Mission Control Center (SCF) 

was 15% completed. 

VI. TRAINING 

Crew transfer training conducted at Wright Patterson AFB was 100% 

complete. Other crew training and tests involving NDAC-ED were approximately 

50% complete. 

VII. NANAGENT 

MDAC-ED was 44% complete with its input to the MOL Easter Schedule. 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

Statement of Work - Status as of 10 June 1969 

MDAC-ED 

Para 2.6.1.5 Authority UM201 

TASK - MASTER SCHEDULES 

The task was on schedule and was being performed in a satisfactory 

manner. At termination it was 44% complete. 

Para 2.6.1. 1.5 Authority N-25-15.0/M 

TASK-PROBIa4; ANALYSIS REPORT 

The task was on schedule and was being performed in a satisfactory 

manner. At termination it was 44% complete. 
-,- 

, r,,,7, 4cC'''',Z „,...E777,7,.. 

fc..... 

,.."..r_ 

^ 

c.... — 

,......, 

•-• 

.. 

.. 

c=strzio.. ....r.facaszscomm,c..-.; 

.7.* 4* aft 

N a Cs4 . a 

„,- 

X _ ci :Jr; 

t. o 

cn 14... 01 - 

p 

'O. 

...

z 

..• 

, 

. 

G, 

ra 

•-• 

../7 

..0 

' 

X 

,•C 

. _. 

4..... 

C. 

7e 

0 

N 

.c 

-. 

L._ 

.. 

o 

..i 

07..... 

' I i t " I : I i i 

— 

- _ 

_. 

C - 

vr 

u ,I7 

•C 

= 7.7., 

-.- 

CC 

.... 

_ 

. 

2.. 

••• 

X 

.... 

. 

•• 

..: 

2 

. 

1 ,1F,PA A M 11 AS.0W0; 11,105-111 

1970 I 19 * CO 

.- 

c:. 

I-- 

- 

- 

07 

.--. 

e .... 

cn 

..- 

o 

- 

i 

_._ 

i 

ae 

,,, 

17 of 

•11cJI:i 1 13 MAR: • 

4 . i_ 

:151AN1.1. 8A5 

- 

. : ■ Z

1 

‘`..9 AIRY. 125 MAR: ;

.. 

f---- 

'-...':01" - 

•- 

...i...Z X_,O., 

cr) •-• 

'-,.- 

r„;, 

*-,. 

.. 

....„ 

Z 

- 

C. 

V) 

•IC 

CO .7 07 -. 

...... 

x 

x, 

... 

1:7 

Z., 

i. ., 

4C 

_ 

...., 

Ca' 

co z 

.- c. 

- . 

CO 

p.. 

. x 

74. • •• ••■•• 860. • jr ••I. ••• . 1 I. 

• T•..i. Immo ii• 

'-;r•Z 

Cr) • 

• 

.... i* 

g .: 

 1... 

...- 

0, 

GO 

•-- 

, 

I 

.• r, 

I 

.- 

co , CD,7 01• 

r- to 

...... 

op 

CO 

• 

4- 

0.,_tiD4 1 ;F :M:A,M,) 1. 1170;0 ;N0- 

_ 

. 

• 

.--, 

' 

cr, 

.-- 

- 

4.3 AYE-3 MANNED 

4.3.1 ASSEMBLY 

43 2 SSTL DELIVERY 

4.4AYE-4MANNED 

441 ASSEM Y BL

..4.4.2 SST & DELIVERY 

MONTHS FROM_ EDP ATP 

MGNTHS 

CALENDAR YEAR 

FISCAL YEAR FISCAL YEAR 

' ACTIVITY 

CALENDAR YEAR 

MONTHS 

MONTHS FROM EDP ATP 

01.ENGINEERING 

11 DRAWING RELEASES 

111 REENTRY VEHICLES '" 

11.2 A CAPTERS 

I2 CRITICAL DESIGN REVIE1V-START 

12 1 AVE 

■ 

1 

..- 

.- ■•.,

- z._ " — — 

es 

02.GROUND TESTPROGRAM 

- 

2 1 ELECTRONIC SYSTEM TEST 

22 STRUCTURAL TESTS 

22 1 ADAPTERS 

222 REENTRYVEHICLES 

... 

pr — 

E 1 

.. 

ur 

ni 

i 

z 2 

.. 

..r 

73 

.-:_- 

73 

.. 

.., 

N.- 

''''' 

— & c3 , 

* E 

a-- , •-• f. ., 

o s x 

. 

....• X 

n 

5 c. 

- = 

a x 

LI 

., el 

en 

' 

"` 

32 2 DELIVERY 

33 COPS MANUFACTUP.ING. C 0& DELIVERYi 

3 4 INTERFACE SUBSTITUTES 8 U & DELIVER 

04 MANUFACTURINGAND INTEGRAT N IO

41 AYE-I 680 

411 ASSEMBLY 

4.12SST 1 DELIVERY 

o 

..:. -. 

. 

"/ 

sr 

sr 

mars 

422 SSTL DELIVERY 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

CONTRACTOR: HAMILTON STANDARD 

STATUS AS OF 

10 June 1969 
NRO APPROVED FOR 

RELEASE '1,JULY 20 5 

STATUS OF HAMILTON STANDARD EFFORT AS OF 10 JUNE 1969 

I - TRAINING PSA STATUS 

1. TPSA 1-9 have been delivered. 

2. TPSA-6 has been returned under the correction of deficiences clause 

for a fit problem. 

3. MA-10 has been rejected due to fit and function problems and is late. 

4. TPSA-11 was acceptable with consideration of Airlock electrical 

housing worth approximately $1500.00. 

5. TPSA-12 is late and is unacceptable for the intended crewman due to 

improper size. 

6. TPSA-13, 14, 15 are complete but have not been presented for acceptance. 

7. Hamilton Standard has been notified of the intended crewmen through 

TPSA No. 18. 

8. Parts and components on TPSA 10-21 should be in some stage of completion. 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

II - DEVELOPMENT PROGRAM 

The development program for the basic Pressure Suit Assembly, prior 

to the implementation of the fire proof non-metallic materials program, 

is essentially complete. 

One month of testing remains to be completed on the helmet drink 

port. Target completion date was 30 June 1969. 

Two months of testing on the absolute pressure controller remain to 

be done. This testing was to be conducted from 1 July to 1 September 1969 

during the Dual Gas Test at MDAC-ED. 

Additional testing on the Arm Cable Guide was to be conducted from 

1 July to 1 August 1969. 

A11 other development tests on the basic Pressure Suit Assembly have 

been completed. A totally developed PSA could be available with minimum 

expenditure by 1 October 1969. 

Contract Change Notice No. 11, was sent to Hamilton Standard on 21 May 1968. 

This change order authorized Hamilton Standard to procede on incorporating 

non-metallic materials into the Pressure Suit Assembly, Constant Wear Garment 

and Flight Configuration PSA. 
Fi Pt? 

8 

U 

8 

O 

3 q

A 

O 

crr' 

t:- • • 

H H 

ri Cu M 

• ‘..6, cc; 

ri 1-1 H `I:74 

0 

g 

g 

0 

0 

In 

0 0 

03 

0 

0\ 

0 0 

H 

0 

03 0 

I" 

0 

0 0 

0 

c0 

0 

03 N

a 

ri 

N 

0 0 

0\ 

In 

03 

tai u■ 

34 

Pi 

Lc\ 

N 03 

a) 

0 

0 

03 

4) 

0 

0 

0 

0 

0 

N 

N 

LC) 

0 C 

LL. 

›- 0 _1 

1.1.1 

> 

-2 

0 0 

H 

cel 

MM 

Additional 

8 

0 0 0 0 

0 01 04 0 

a 

 03 a) 0 0 1 

CU M 

0 0 

N t— 

GLOVES - Additional 

8 

H R

8 HW Nt i

0 

1st Unit Feb 70 

Deliverable at end 

1st Unit Sep 70 

Deliverable at end of development 

CDR 1 Apr 70 

1st Unit due 15 Sep70 - See Note 1, 2 & 3 

CDR 1 Apr 70 - Note 3 

Note 2 & 3 

Note 2 &3 

10-15 complete, 16-21 started - Note 1 Nov 69 Delivery CDR 1 Apr 70 - Note 2 &3 

z 

CDR 1 Apr 70 - Note 1, 2 & 3 

4-4 H.r4 

O 

41 

1-1 

5 

O 

401 
o3 

0 N 
.... 

•IIII 

IOUs 

' 

0 • ,, . 

I i I ri ■mmiumumm ir 

u

l 

ri 

iii I 6 11 

il 

I I orromumunimir r 

or 

No Iiiimmins 

1 . ■ II 

I I I I I II I I I I 11 III 11 

Ciao tailed SAR - Referto HS latterHSL-566 

11 1 111 1 1 11 1 11 I I III I 

No 111 A 

■ i 

'11111111•1•Illiti 11111111 

III II ■ 

MI MI III MI ■IS . 

5 o si No 

m 

. 

■ 

anions- am. moo 

no al II. 

I NM A NEM 

M1111111111111111111 

Insommo ■ MI 

0 

NEM MO , IIIIIIIMI•1111 

MI MOEN. 2 mourn 

■ an 59., ii iii 

j ounino 

IM 

Nom no ■ MIMI 

I ■ 

111111 

4 

fl I I II 

I 

li 

I 

■IN 

p 

Nm 

■ 

mmmum

sm 

I 

— m 

........r 

a 

Id 

limullurtimeimmuu 1 ; 

b._00 WI 4 MI , 

; 1 ■1 - 11- • • 1 _, la 4, 

r co a no , so WI IIIIIIII 

IIIIII 1 IN 

0 H . NE won NIIIIIIIIIIIIIIIIIIMEIMIMINIMMIIIIIMINI NI 

&IL .. lig il ill FM 0 o rn o. ■ 0. ■ ri 1 

i:,_ 1 g 1111_ 1 ..„- I IN I Iiiutiiii 

70 1[4111111111111111111111111111111111101001M111111 MMIIIIIMIMI •11111111 I. MMIENINISM L ' 0 

1 t-- ' 

g I III lI III I I 

j • „._ IS • MN 111 

7 

: 

.. 

. 

IIIIIIIIIIIIIIIIIIIIIIIIIIIIEMMIIIIMMIIIIIIIIIIIIIIIIIIIMIIIIIIIIIIIIMIIIIIIIMIIIIIIIIMIIIIIII 

. 

. 

. 

IIII 

. 

. 

. 

MI 

: 

: - 

Ell 

la

rnitton 

sta

nda

rd °-°" p 

mo... 111111111: 

., 

• 

. . 

- 

. 

; 

. 

- 

- 

.mO. 

. t. 

,.. 

. 

. 

. 

- 
1 ln 11 1 1 111 111111 i ll 

rEi ). 

u 

.. 

Ile 

. 

liii i m.. l .s

a .. -a 

1111 

1 

aau 

a N 

0 j 

4 MOM 

.5.4 9 R s iIIIII.lihlIIIli 

mit (7,4, mu um 

;7, MI . 

Y 

. 

I

1 

t 1111 IIII MI a 

: tai 0 

1 

1 t. 110-1111 

' 

• 4' III 

rer LI MEM 

M n 

!er Li 

!+ 

‘' •A

1111 NM aaaaaaa uaa a.a ME 

El a 

1 1 MB MINI .1 NI 

. ,,Ittrcoi ME 

to—. V 

il s 

! M 

MI ZI t 

M Rim 1 

I -• • 1,.. "_..., lfl P IMAM ci tI Itt .... 

: ell. I I 

180 ; 41 d dm 1 E • R mum 

ilb 

aam 

u 

In tammummgmmlwrim 

MEIMMAM62 

.. 

1 u I Arm 

As MI AMA 

Em Immumme 

Li Mallaa 

1 

z 

• 

1111•111.T.p..r.p.. Ai m 

4 7,tio Pam. MU Will m: f Id :1111 1111 co - 4 Mt ,4 ma NM ; PI - .:. 0. Ilmn tlf ral

----... a gi .- ... 1 1441 IIIMI r I I k4.. ' 0 ., . 

UMW mi • N. II 11 up N aril 1, 4111 MB E . , 4 Li um El l ri . au 1 r- IN 

..- 

gm 

..„0 

k444 .' aaaa 

, mitirli 

Mill I 

ill 

urnurrormir aaaa ‘'I . aa 

Li 0 2 

l 

Li 

:liurier 

M 

MN er MI 

................... .. 

m mix mucimousommolumsomusimm L., 

•: .11 . r... : 

, . , . 

o ''' Al' 

4.,I 

00

4. 

& 

Ship

mate(Contract) / 

(Actual) I 

Aerospace Ground Equipment' 

Portable Comm. System I 

Shipments(Contract) I I I 

milimmommummommummummummmum 

.4 4. 

O. 

t k 

_ 

C3 

0 

.4 

v A 

.... 

CJ 

0 

-. 

,, 

.4 

4. 

(4 

. • ' 

liLmilimm m 

tia

msiton 

Sta

nda

rd 

u. 

. 

I ! A 

0 

_ 

. 

Shipriente (Contract) 

Ememency Oxygen System 

A A 

WO 

' 

4..H ■,.., 

7. 

.1 
6 im ow lawrai 1:1 MN& IN sr ,,,.3 s mull 

III 1 1111 1 a 

I / \ hiblE III'S M 1111.1 a■a I lis 

- sus ia-anuo lommuormlimms% 1. 

mum 

mirmaimimi 

El ktfr,". IN NAN= 0 7,14 mum: mommummom wwwwwwm Na 

I 

woo 

■1 

01110wwwom 

1 c, ., _ ME in on so no w pima! 

"

■a 

. 41 a MWII ..,. 

ra DI 

ir 

NOW 

■ 

■am SI 511!• aaa A M§ NM III qi DI gillii kru, ■aa R Mil si MIMii Ili: 

ma ■Hi a' i lE 

iaa 

Earl 

mom no m 

• se Emiumiz lik, -14 .1 R 5iiiimminuomummism gm MEC 1111k 411111111111 tri 

S NMI i:13 M EN ir: 

, 2 gig El ■NI Dri M. i„, t 0 unikummummorm as 

NI el ■ ■ 

nous. MOWN • , MN I. El fa a CS ■FS ■El ■I:Rilg 

, imi ■CO ■ IN Kiii Km IN ■I:W. ■Myr on ■ , ra ■m HIM Pli Rfi KEW: 

151 

,, 

NTS OM MI IS M NM% 

, '.! 111511 ■ IN ■ ,, 111 

0 kA ,, II a 

. Inumnoments El mummanuomanus el , m si IN mu

,.- 5 w on inw WW 

X , mm NW 1111 Mimi wro I mull, 

CI •.,:; essianummenumi irmusurnamos No mo mi. %1 gm :a 'am 

• EMU MI ki ■qv xis 'mu 0 ,,,,. ■ —En RI C43 41111 21 I 4 I ■,* 0 ,, az, Ka m MI IM W

m 

■ 

E 03 0 . 

. %, 

-. 

:es 0 a mom ■m a 

LI 1 kkjil IN NI am IN sammammmumoom a ma 

rrto 

< 

m 

° 

03 

'■I 

a 

'. 

kiii 

titio.A2 Itklo LI II IM 

Ram Ivanammommumaminamframmirmumomammums 

Wl:i 121::::::::::::::2::::::Imararl::: 

vl. 

a 

W 

"r e- mmmoommmumw mon im m wi mom m 

...., 

a Li. _ •,, El - r43 III 

g . • t■13 wiummumma- m iswoorEiw t ww no al ww woom In mom mom - 0 g .,.- . IIIIIIIII I : em MNIMINICIMIleigrIMONIM ' 1111 

a :: ,,, till ■WM 2 :4 Ull ■ r4 :MI 

C • LP1 ■II 4= ita MIN BEl as 

0 

Z 

° 

; 

6 

. . INmg 

*4011111111g0111111011111 :41 

PERM 

 • 

Bow .............". R 

11111111111111•111111101111rr 

Ed r 11 

NIL 

eil 

131111111111111111111•11111111111111111111 III 

I - : 1111 IIIIIIIIINEMom 

tli : ... .. 

LW= r-, Fin EMI 

wr 

. -mM In El 111111 Mil MOM IN MEM 

• ., 11111111m1111111MmunnommommmillmmulommlMMIMMIN J., ■MIME ■MIMIN 111 II 31111 SI :.. Mri iwsni 1 111111111111 ■III EIESIO4 

1 

1 

kf411. 1

hi.... n . ,...,, 

i 

., 

(Actual) Lil 

(Contract)I 

.., 

RIM 

Willi o ,,,. 0 .e 

SI 

1 

. .,c 

(Contr

.. 

actM 

Ili A U 

111111111111M11111111M1111101111111111111111114MLIQUI111111111•1111111111.111111111UUMMiki 

...., 

1J C.) 0 

.t 

, (Contract)! II H astual) 11 

6 

, 

■-, 

11 11 

Ai 

I ( Contract) Un1-1--- l(Gontra 6T-T 

F1=11 11Mal I 

Sta

nda

rd 

.14 

• 

g 

ImmersionProtection SysI 

fC 

Urine Management SystemI 

0 

MaintenanceGround -•ui•. 

Ground Maintenance Rit 

]round Controller 

• 

Y4 

i 

F. 

0 

L-. 

- A 

8 

I 

i 1 
MO 

1 1 ii 

r --r Ng 

m II m mrim 1 1.••••■mamomilmEN imusimi Immusammommlimmod111111111 

INN IMMINIUMMINIIIIM11101 ill 11 1111111111111111111111111111 mi 

•MI 

1 •IMN 11111111 a IN •••■• NEM or' ma Is a Im 

mommumom mumm 

no m mum= mum 

som ma maim m m m m 

m m sem 

ma 

III a iammammummumnousamommi IN mi 

am • 

mommommum m 

m 1 

on 

I am mi m m mommomm m um m 

1 

'1t 

:4,.. 

6 

kr*_1111101111111111116111111111111111111 

IF 

il Ill 

11111111.1111•111P•11111111M11101111111111111111111111111111111111111•111111111111111111111111111111111111111111111111 

1111111111111111•111111111111111111111111111111111011111111111•11111M 

11111111111111MINI 

IIII 

II "i1111111111111111111M111111111111111111111111111111111111111111111111111111111111•111rnalIN 

MIMS 

11011 Ig II 44— MN . IIIIIIMERAIIIIIIIIIIIIIIIIIIII NM IIIIIII MIMI 1111111111111111111 MIMI 

MiZi 11111 

2

SA 

tr

act 1 

-grArAi 

kbAMOMMOMMWMT 

rag um 

• 1111111111111111111MMEMINIIIIIMEMPIMMINUNIII 

411 

,_, - 

1111111111111•111111111 

IIIIIIIIIIIIIINIIIIIIIIIIIIIINIIIIIIIIIIIIIIIIIII 

111111111111111111111111111111m le 

ni Ems x WWI. " 111- 1 

., 

Nillill 

am 

MS mountommummmummommmommumm 

ow 

1 

IN 

mi 

aummommommom 

ummummum no woonmommumm 

LS 

, NM 

. 

N

.... 

.. 11.11..111.111.11.11111111111111111111.111111111111.11101.111MOHNINEMENIUMMI 

. II 

1E1;1' ( Contract) 

(Actual) III 

a. 

PAIIMIIIIIIIIIIIIMIUMEHIMMINEINIMMINMENIMMOMMINIMMINIMEMEMINIUMUNIENII 

II II II 

Ha

milton 

Sta

nda d r i 

F: 

. 

(*For Dual Gas Teat) 

• 

A Neck •Lt..t Retro 

ileetric Harness Retro 
, W 1•••• •-• •• Iyo7 196b 1969 1970 1971 1972 

, "1. 414 9 /0 747

,0 7044, 04/04 Vi4V4 440; 4/

404 OP/ 

.. II . ■ 

. ... III mi mu.. es m ..1. m 

. s Li m III 

.............. milimm im . mill 

• mum mum Immo implumm.... 

mmmummmmmmmmmmmmmmmammum mmmmmmmimmsmmmmmmnmmmm m 

E WE 

um • Is milli ill mom' In 

um mill mum 1. 

IN Es a m m m EE 111 

E ME • MEMMEEMIEMME MEM MEM 

ME • MI MI E MEE MENNEN.= EMEEMEMEMEEMMEMEMMEEmEME MMEEM 

..... MEE ME ME E 1 . 

• . . ma . 

........... .......... . .1 . . . 

.... .... 

... . • ■ 

.... .... ....mu. . ME ME MEM ME EN ME MI E E 

• E El 

1 

El IS EWE 

• MMEMEMEMEMEEmilmEMMEMMEMEEMEMMEM 

111 E EMEMMEMEEEEMMEIMEERE EMMEMMEMMEMEMMEEMEMEMMEME MEE 

gi mmommommilm ME MEE WEE III MM 

MEMEMEMEMMEAMMEMMEMUENNIMMEMMM M Eril 

EMEINOWE ■IMMEEW 111EIMEMEME 1 Id 

.....................m MEI • 0... FIII 1 EEEMFE .m.L.m... 

K 

A KW . 16.1r

nm 

.... ;.. .1 

pm AMER NM Imml 116 E PE 

- W ■ 4111Ki KliEU E 

W ■k ■ u lb■ 

mrammommimmulmomminumm mum mu 

m ■imil k mos mon 

ir# lik 161 % 

m mml mmmmmmmmmummmmmmmmmummmmmmmmmmg 

■

m immil ■MEEEMEEEM ■EEEMMEMMEMEMEE ME 

EN E E M 

.... .............M. MEM EMI 

, 

■ DEVELOPMENT TESTING 

CCN ill 

. 

1 

aC 

• 

• 4 

4. M 0 ft4 

0 io .-i U Y 

.. N 0 

e 0 R .. 0 • 

o W 

y 

• 

. 

• 

: 

. 

(HS) Gas InletConnector 

M 

2 

_ 

z 

M 

H 

Zipper 

. 

M 

( HS) Drink-port I 

(V) ABS Preen. Contr. I (V) EOS Connector 

(V ) UrineMgt. Syst. 

(V) ImmersionProtect Syl 

. 

e 
IDATA ITEM (U)f % 6.

.11 

It41 11 I II I 

0,14 II ' .ISIE 

I II II i - II ■I11 

kill II 1 1 1 

4 

, 

III 

0 1-68 

4 4 

1 4 4 

11 0 . 14 1 I 

II I I I 

1111: IIlIIIillilililiiillli 

iiil 1111 II II I 

§4M 

1 I 1111 

1 I I iiiiiiiuuuinii 

■ I 

•••••• • " •• • ammo. oruvrr Sta

ndard 

'easibilityTesting 

p. 

OvermisorHood 

ParachuteHarness 

14 

Development Components 

. 

2 

1

. a

v q 

ri 

. 

Electrical Harness 

,Fl 

Cycling (D-3) 

. 
.— 

0 a 

>- 

LL

o 

w . 

> 

LU 

g.' 

0_ 

cn 

< . 

o :23 1 1 

w , 

z 

kill- W11•11111 1112111211111111 

11111111111111111111 

ITIIIIEIMIII I IIIIM or LIMII 

• ......ini, MI 

• 

• 

MI UMWMM. 

EL 

Ili' 

-1,, 

at 

• 

• 

• 

11111•111111111111E1 mu- •

al in 

MI M. mill..m. awinueum. Num 111•1 

.• DATA ITE 

14 -

4 

,e,, 

400 

IMI 

1•1111111111111•11111 

a 

MINN 

IN al 

11111111111111111=11111111111111111111 

IMMO 

11111111111111111111111111111111111111111111111111111111111111111111111111111111111111111111111111111111=111••••• 

wimornM111111111MMUMMENNUOmmiumumniNEMNINUW 

M111111111111111 

M111111111111•11111111111111111111111111111•1111•••••••••1111111111111•111111M, 

IIIIIII 

• 

MI 

• 

Um El 

. 

MI 

MI 1111111111111111111 III • MI MI Mt 

It40 MIMI 11111 11 IL 

MEM EMI MOM NM In MIMI MOW 

• mit 

IN: 

; 

: i I 1 

 I 

I P. E. KLISIEWIC 

h,, 

lk, _MI 

kt,._ 

qi•••••••• 

104111111111•111111111 

tre411111111111111111•1111• 

N mum.. 

• 

lum••••••••• 

• 

IIIIIIIIIIIIIIIMI • 1111 11111111111111111111111111111.111 MI 

• Nel fu 

RN 

am am• IN Ra. • IN 

mum mum um II 

IIIIIIIIIHMMIMIIIIIMIIMIMIIIIMMMIIIIIMIIIIIIIIIMIMIIMIIIIIIIIIIMHII 

• 

111111 

1111 

MI 

MI MI 

IM 1111111111111Mali IP 

Mk _

mi. 11" 

so 

ME 

ill ••••••••••• Nou...........m.......... mi. 1111111111111 NI mil • • . 

me ma a 

.. 

is mu • 

•••••••= LI • k44 a J 

-. 

, 

• i' 

.. ..0. 

IIIMMIIIUM111•111=1111111 moms le 

MIN MI III III MI IL • 11111111111111111111111 1111111111111 MI MI MOM II MI • 11110 12 

f_FI 

a 

% 

tt444 .. 

... 

. MI IMMO 

mew iminus 

• 

4"A:se 

•• • 

• 

• 1111 

• • 

MILT 

•••• 

• 

II 

. 

11111/1111111111111.1311110111110.11111m111• II 

NI1111111111111111111111•111111111111111111111111111111111111111111111111111111111111111111111111111111111111MMI 

innumummommumminumem 

5.• 

IMSAMMIIIIMMIIIIIIMIIMIIMIIMIMEIMMMIIIIIIMI 

mlum. 

•• 

MI Eq. MI 

K. MN 

LI 

MI ., I 

I" mom 

a 1111111111111111„ 

IIII•1r, 

MN NM 

mai 

Nal 

t 

• 

lit 

II 

imi 

MI 

E 

L: 

2; a 

I 

• tt-wf,11. !tali ."‘• II 

• k_MJIMMIIIII is minsimilm 

me 

MI MIME 

wommummuni 

RE 

ILIII mg 

• CI 

orm 

• 

1111 LI 

INN 

• 

41.111111• _„„ 

• NI 

MI 111 MI ME • 

C 

0 i 

C41 

- . 

*A 

gily& ' 

• • 

IMIIMMIIIIIMIIIIIIIMIOUIOIIUMOHOIIOIIMIIIIIIIIIIMMIIIIIIIIMIIIHIOMIIIIIIIIIIIIIIIIHIIUIF 

•• • • 

NI 

.? k,,, . . . . . 

• 

a_ 

I- 'IP 

IL 

•, 

al 

. 

IIMIIMMMIIIIMIIIMIIIIIIIIIIIIIIIIIIIMIIMIIIIIMM•IMIMIIIIII 

MIMI IIII 

al 

MI 1111111111111111111111111111•1111" Ilk 

< MO 

4. 

,:t 

. I 11. MI III - 

° g 444 - a z i• 1. IN mi im 

0 ipz 1, • al al mu. or A k) i; . mommum 

"m4sminursumniummuommusimmEmmummum lam IN 

NI IN 

ilm 

ammuunnions Nummus 

,, iinummums Num No % ••••• In C kii (4 I, 

111 .. IN NI • • Nu a at k 44 4 mum sul • ...mmimens I. • • 

.4". 

: 

.1 

MI MI 

• 

II 1411111•111111111111111.1111111111111111111111111111110111111111111111111111111110111111111111•11111111111. 

• 

• • MI al 

11111111111111. 

I 4:-. INEN 1••••••• • al • • 

. 

kg.. 

MEM 

is MIIIIM1111111111•11111111111111111111111 

1111•1•11111111111111111 

insiou 

ili 

NI 

/ 

IN 

MI 

IIIIMIIIIIIIIIIIIIIIIIIIIIIIIIIIIMIIIIIIIIIINIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIIBIIIIIMMIIIIIIIIIIIIIIIIIIIIIIIIIIIIIM 

vs;;111111•11•11111•1111111111111111111•111111•1111111112111111111111111111111111111111111111111111111111111111111•111 isi 

NM 

1111111111111111 

irm 

1 

al 

MI 

MP 

III 

III 

11, 

111111111111111111111111111111111•11111•111111•11111111111111111111 

MCI V 

3ta

ndard 

- • 

I 

• 

0 .0 

a 

S. 

P. 

0 

= 

0 

r.• 

- 

.i 

Functional GroupE 

'4.‘ 

n1 0 DI 

0 

0 0 & 

1 

0 

.4 • 

... 

. 

0 

r4 

Urine Nget. Syetes I 

0 

0 

„ 

A. 

' 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

TITAN III M 

STATUS 

10 JUNE 1969 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

T-III M 

MARTIN MARIETTA CORPORATION (AIRFRAME CORE) 

AVE: Basic design 83% complete. PDR complete. CDR complete. 

COMPONENT DEVELOPMENT: Computer 71% complete. Actuators 75% complete/TARS complete. Static inverter 97% complete. 

M-1 FABRICATION: No elements started. 

AGE: Basic design 69.5% complete. PDR 94% complete. CDR 71% 

complete. AGE fabrication 50.8% complete. AGE delivery 61.8% 

complete. 

CAGE DESIGN: Complete. 

AC ELECTRONICS DIVISION (INERTIAL GUIDANCE SYSTEM) 

AVE: Basic design complete. PDR complete. CDR complete. 

IGS DEMONSTRATION: MGC qual test complete. Signal conditioner 

qual test complete. 

AVE FABRICATION AND ACCEPTANCE: LMV (new build) not started. 

MGC not started. Signal conditioner not started. 

AGE: Basic design TDMG complete. PDR complete. 

CDR COMPLETE: Fabrication and acceptance - TDMG complete. 

ACTIVATIONS: ETR guidance lab modification complete. ETR launch 

pad AGE modification complete. WTR guidance lab not started. 

WTR Control Center not started. Denver lab complete. 

UNITED TECHNOLOGY CENTER (SOLID ROCKET MOTORS) 

AVE: Basic design 50.7% complete. CDR 93% complete. 

COMPONENT DEVELOPMENT: Structural testing not started. Hydroburst 

testing not started. Component qual test 68% complete. 

FABRICATION: Cases 29.4% complete. Nozzles 33.7% complete. 

DEVELOPMENT TEST: PFRT not started. FACI not started. SRM deliveries 

not started. 

AGE: Basic design 71% complete. 
NRO APPROVED FOR 

RELEASE 1 JULY 2015 

AEROJET-GENERAL CORPORATION (LIQUID ROCKET ENGINES) 

AVE: Basic design complete. CDR (Stage 1) complete. CDR (Stage 2) 

not started. 

STAGE 1 DEVELOPMENT: Frame complete. TCA complete. TPA (turbine 

kit) complete. Ablative skirt complete. 

VERIFICATION TESTING: TCA complete. Engine demonstration complete. 

FACI (Stage 2) not started. 

STAGE II DEVELOPMENT: TCA 94% complete. 

AGE: Basic design complete. AGE delivery not started. 

LAUNCH COMPLEX (SLC-6) 

The Martin effort at Vandenberg AFB in support of the MOL Program to 

10 June 1969 was as follows: 

a. Support to the AFSC Civil Engineers and the 6595th ATW for 

construction surveillance and validation test review. 

b. Secretariat of the Facility Working Group. 

c. Maintenance analysis for the Real Property Installed Equipment which the Martin Company was to maintain. This included writing 

of preventive maintenance procedures, spares level determination, 

procurement of spare parts and technical representative support to 

the military maintenance team of AF accepted SLC-6 facilities. 

d. Launch operations planning, including support to the Launch 

Operations Flow Subgroup and Launch Operations Working Group. 

e. Activations planning, including secretariat of the SLC-6 

Activations Working Group and integration of all MOL associate contractors' SLC-6 activation effort. 

f. Technical inputs to the SLC-6 Communications Plan. 

All support provided by the Martin Company in these areas was considered satisfactory and accomplished in a professional manner. 
1E1 

etz 

F— 

69-SMVTP-16 

0 W 

0 a 

1:4 < 

co Q co ,•1 ic) 0. -0 

Uu 

Uq4 

W 4 c4 

51 

a, a 

v~U Z 

t 

O ° u_ 

[1. W a. u) 

< < 

0 _I 

X W Z 

I 

1-11Th-Ti=f-11-1 ] 

J A S ON O 

0 

., 

, -. 

, 

— - 

0 

= Q 

.1 

. 

,.., - 0 

, 

>.• . No 

ITT-IETTT3/4-1- 

IJ FMA NJ JASO NO 

r., 

(ii 

0 

Iy 0 

- 

nt 4 

N 0 

= 0 

•at 

M i 

N U. 

N -. 

>. 

IJ F MANJJ A SON O., FAIA UJ J A SONO 

CP z 

Ca 

an 

,.. e.i 0 

0 

= 

4 

ea. 

>. . 

0 '0 0 1111 

„, Emmeuminum.r,i sommune NEMO 

0 I i, NM EJMEMMEM EMMON____ 

rfll El 1,01F1 h. El is. 

- grommimmom. 1.111111•1116011 ' In i ICUMNIMM.L.111/ 

0 IMMETIAIM EMI i 1.1_.111.11111=EMEI El 

.., r I MEN AMENIMIUNNEINI 

FY 70 

m 0 4 mown um - Numumioun 

._ wilmmiu IN , . summummu m 

, T1 t . NIMIIIilli i MI ' MN 1 --. , --T ,!,__,. 

, , ,; i, EN f t , j MI 

.1 2----1-1-n- f r-11_,H ! j MM. ; 1 iMMinall iii 1. 

- r 

177 MUM 

o --i :.1 rhi t 1 :i tii_ INNIONIEHNEMI MEMENHE 

.> i i ;, 1. : : , i ' 1r I i 111.11111.1==.11.0 r IMMINNINIEEM J` 

, 

!. • i'l 11 INEMENIMINIEM MEMEMINEMONUE 

FMAIAJ J A 

; f

ri 

NUEMOINI ENUMEIMMEN ,Ili t.) = i , • r, INENNEMONIEMILO t MEMNON.= ' 

... • . i ._i ; NIMOOEININOMEMM "MMIIIMISNO 1. i. EMEMONOINENE IMEINEMEI i 

,,,- p r S I . IIIIIIIIIIIU•MIIIIIIIIIIIIIII1 1•111111111111•11111 

T-1,i i .1111111111111.1.11 I" i 1111111111111 c 1 v 

. 

di J 

>. ct, Ci i 11.11111.1111. E i.= MUM 1 fr ' ,,4 4 C■ 

44 

= • Li : - 1 11111.11.11..1.1111111111111 MEM t t----4 —1 ! I: z 

o f 1:2 T MR NOMMENIMEENI NMEMINEM / r j___I _, j I, 0 

... 1 i !'1. MI INEMINIMUMME NIMINNEE .^ 

= . 

'' L f.i cra 

•at 

e ti , =IN 11. 1.11111111111111H11 4 MIMINOMMI ' ' 

'' -' e -L: i IMIONOMME I IIINNONEUE i . /.;: -, 

>. -, i i',I ME MIOINNIME / :.t. -, 0 L ! 1.111. 

EIMMINVIIIMEM 

MI 111.111111111111 1.111111M110. t t j. t. 11: ; It M 

.3 ' L ; El 54 54 ME•54 Erni MiniiMMO 54D tj 4 w i ' ii 4 

M I L, 1.1 E. E. F. Mai t INSEIMMIE c-. E 4 ■ I E. 1 i 11 m 

t... i 41-1 I i 7 1‘1 14 iiini 41 IN Minell0.11.1 41 4 ri rw t li '"- 

-. o 

= 

.1 a a a, ...1 1111111111111111111111•11 q, -4-: • a i I LLO 1 U....__.... 

FISCALYEAR 

CALENDAR YEAR 

MONTHS 

AIRFRAME CORE (MMC) 

Design Engineering 

Component Deve lop

mentand Test 

QualificationTest 

ControlsM/UTest 

F. 

--' 

U v 

il. 

AirborneFabrication 1st Article 

VTF and Delive ry 

AG E Production 

INERTIAL GUIDANCE SYSTEM (

ACED) 

DesignEngine ering COMI 

QualificationTests 

ComputerDelivery 

). 

. a 

Z, 

:1 

a 

I. 

'! 

§ 

.. 7 -5 0 

7'o E 

AIL 

>. t1 

> 

-; 

-c 

e9, 

., 

,,i 

c' 

L AGE Production (TONIC) COMI ISOLIDROCKET MOTORS (UTC) 

DevelopmentMotor Firing PFRT 

FlightUnitDelivery, 

AGE O/D VAFB 

LIQUID ROCKET ENGINES (AGC) 

StageI TCA Develop

ment CO

M I 

TPADevelopment 

ExitClosure Develop

ment 

DemoTest • COM! 

I Stage I I TCA Develop

ment 

Den-lo Test 

I LRE Faband Delivery(

0/D AGC) 

AGE Production 

ILAUNCH COMPLEX (SLC-6) 

(COE) Construction 

Equ ip

mentInstallation1StGST 

FLIGHT SCH EDU LE 

PAGE 1 OF 6 
H 

Z. 

41 

H 

Z 

0 

0 

1 

0 

0 

A A f4 

N g 

a, 

A 

NI 41 4 H 

41 o H 'E:8 ;n 4 

O 4 4 

z 4 0 0 .-4 

P, 4.1 r4 

V) 

NI 0 U

a 

 0 

> z

w 

4c 

En < 1 cf) (r) 

6 PQ 41 

E-4 

41 r11 .

E-4 

N g H • :f4 :`z. 4

A <31 W 4 -.. 

n .4 (..) A .--, °-1 

< 14 0, H En 4 

4 v) 4 rx1 El E--4 

41 

v) U

.-1 ,..4 O H 0 0 0 

H Eri •

41 0 ,-1 

0 Iv 

i 4 1 1 

Z En 

41 0 . 

> o () 

ai t■J 14 w

zw

• 

a 

14 

> 14 MI 4 14 (f) 

c4 n 

o fil 0 to 

41 En 0 

H H 6 0 

c4 

• P4 14 0 

O 41 H Z H Z E--.1 41 41 

1=4 .

11 0 z ,0 —.1 0 ›e4 

O. 41 . (r) 14 41 

41 r4 8 › H ..:._ .. 4.1 

W c4 0 W 

4 

0 

O 0 

O 0 MI 4 0 Z A n H 

>4 H 41 ,,--4 41 

O a o ..4 4 Z Z En 

O <4 <4 < 

.-4 40 

c4 f-T4 

0 

44 0 

a A 04 z n 4 

0 0 H 0 41 L) N 01 as o o 

Z 0 

X 0 .1) r- rO c4 0 ,-- >4 >-, >4 

O 0 0 En Pi En A 44 44 44 

X 0 

• al ric) c4 z 4 r4 >4' 

tsl 4.1 14 0 El :D 

4 r=4 v) A 44 0 A 1-1 

.-• N r") Lr) N co a, I 

!Li 

DUCTION EXERCISE - 

FY70 BA

SELI

NE SCHEDULE ESTABLISHED 

)- 

CC -0. 

4) '0 

0' 0' 

.-4 ..... 

0 _i LLI 

> = , 

ce 0 .0 rs. 

.0 

%

•D % 

lii c)

0, 

v■I 

Os 

/3 

ON 

I...4 .% Et LU 

Z CC