A Case Study in NASA-DoD - The Black Vault

More documents

Recommendations

Info

'I FI Table A-2 SPACECRAFT COSTS WIT! ADDED CAPABILITIES: UPGRADED AEM AND L-AEM-l ($ millions) Maximum AEM and L-AEM-BL altitude = Ceosynchronous AEM and L-AEI-BL orientation = Earth and sun Payloads 114 228 Payloads/spacecraft 13 6 13 6 Spacecraft Type Cost AEM 17.1 33.0 37.8 59.5 STPSS Nonrecurring 22.9 22.9 26.9 26.9 Spin -- .- 31.6 27.2 Low-cost 32.3 32.5 25.3 44.7 Precision 38.2 38.4 45.1 53.0 Total 111 127 167 211 AEM 12.2 26.7 46.1 66.6 MMS 56.1 73.4 65.4 127.6 Total 68 100 112 194 L-AEM Nonrecurring 11.9 11.9 14.5 14.5 Baseline 52.2 85.3 67.6 115.8 Spin .... 14.3 31.0 Precision 27.3 25.9 31.1 34.7 Total 91 123 128 196 AEM 2.3 6.9 11.4 16.0 L-AEM Nonrecurring 11.9 11.9 14.5 14.5 Baseline 47.5 72.7 54.6 91.2 Spin .... 21.6 31.3 Precision 27.4 26.2 31.3 35.1 Total 89 118 133 188 L-AEM Nonrecurring 11.9 11.9 14.5 14.5 Baseline 35.5 85.1 52.2 72.5 Spin .... 3.8 10.8 Precision 17.5 25.9 21.0 26.9 lOS 33.7 -- 58.5 142.5 Total 99 123 150 267
-112- 'Fable A-2 (Cont.) Payloads 114 2128 Payloads/spacecraft 131113 13 6 Spacecraft Type Cost AEM 2.3 9.1 11.4 20.5 Nonrecurring 11.9 11.9 14.5 14.5 Baseline 35.5 60.3 52.3 72.5 Sp~in -- -- 3.8 10.8 Precision 17.5 27.1 16.4 20.8 MMS 25.5 16.5 34.3 80.4 Total 93 125 133 220 L-AEM *Nonrecurring 9.8 9.8 11.3 11.3 Spin -- -- 14.3 31.1 Precision 86.9 123.9 108.9 168.3 Total 97 134 135 211
Page 2 and 3:
LEYEL r o R-2619-RC May 1980 Standa
Page 4 and 5:
SECUNITY CLASSIFICATION OF Twa PAGE
Page 6 and 7:
Standard 5pacecraft.ProcurementL_ A
Page 8 and 9:
-ivas representing the official vie
Page 10 and 11:
the missions required. Third, the p
Page 12 and 13:
ACKNOWLEDGMENTS I gratefully acknow
Page 14 and 15:
-xii- VI. APPLYING THE NASA-DOD COO
Page 16 and 17:
-. - am~rumn -xv- TABLES 1. Nominal
Page 18 and 19:
-Xvii- 11-19. Case IV(N)...........
Page 20 and 21:
-xx- L-ANX - Large Diameter Applica
Page 22 and 23:
-1- I. INTRODUCTION The National Ae
Page 24 and 25:
-3- development. Finally, the polic
Page 26 and 27:
-5- of which spacecraft would enabl
Page 28 and 29:
-7- II. U.S. SPACE PROGRAM: DEVELOP
Page 30 and 31:
-9- thought. (8 ) The launching of
Page 32 and 33:
-1- had shown great alarm or acknow
Page 34 and 35:
-13- for other purposes. ,(15) it w
Page 36 and 37:
-15- and that determination as to w
Page 38 and 39:
-17- program and the coordination o
Page 40 and 41:
t -19- legislation, messages, petit
Page 42 and 43:
-21- of the continuing Soviet accom
Page 44 and 45:
-23- Subsequently, the Director of
Page 46 and 47:
-25- to be asked by one of the agen
Page 48 and 49:
-27- space systems; operational sys
Page 50 and 51:
-29- no near-earth orbit manned ope
Page 52 and 53:
ImP, ~ ~ ~~~~ ......... ~~~~~~~~~~~
Page 54 and 55:
-33- 5. Using off-the-shelf, space-
Page 56 and 57:
-35- 1. Spacecraft configurations a
Page 58 and 59:
-37- STANDARD SPACECRAFT DESCRIPTIO
Page 60 and 61:
-39- The payload cluster, while uni
Page 62 and 63:
-41- payload or propulsion, is abou
Page 64 and 65:
-43- z z 0 0 - 0r CL 0 E 4 41- u- 0
Page 66 and 67:
-45- The STPSS can carry a nominal
Page 68 and 69:
i -47- orbit-adjust module, while t
Page 70 and 71:
-49- M9IS The basic MMS, summarized
Page 72 and 73:
-51- 1980-1990 time period are divi
Page 74 and 75:
-53- about 7.5 payloads per spacecr
Page 76 and 77:
-55- 0- - - - - - - - - - cc - - -
Page 78 and 79:
-57- STPSS (STPSS-LC) spacecraft ca
Page 80 and 81:
-59- Table 7 ESTIMATED UNIT 1 COST
Page 82 and 83: -61- Nonrecurring Costs. Nonrecurri
Page 84 and 85: -63- where SRU = Service Rendered U
Page 86 and 87: -65- IV. STANDARD SPACECRAFT ACQUIS
Page 88 and 89: -67- The costs associated with thes
Page 90 and 91: -69- to increase to 13. That was fo
Page 92 and 93: -71- 500 * STPSS 400 AW-STPSS PROGR
Page 94 and 95: -73- The implications of the forego
Page 96 and 97: -75- option. Other candidates becom
Page 98 and 99: -77- the Air Force's Space Test Pro
Page 100 and 101: -79- decrease any total program cos
Page 102 and 103: -81- COST LAUNCH COSTS (Millions of
Page 104 and 105: -83- V. NASA-DOD COOPERATION: ORGAN
Page 106 and 107: -85- the MHS program stemmed from t
Page 108 and 109: -87- The Air Force had studied the
Page 110 and 111: -89- Air Force Headquarters to NASA
Page 112 and 113: -91- turns out, NASA had agreed to
Page 114 and 115: also evaluate whether or not adequa
Page 116 and 117: -95- design, mission model, cost es
Page 118 and 119: -97- Force interface was retained,
Page 120 and 121: -99- experience and by identifying
Page 122 and 123: . . . . . . . -.. . . . . . . . . .
Page 124 and 125: -103- the nation and other governme
Page 126 and 127: -105- Appendix A ESTIMATES OF COST
Page 128 and 129: -107- RANGE OF BIDS Item Range ($ t
Page 130 and 131: -109- Table A-1 SPACECRAFT COSTS--N
Page 134 and 135: -113- Table A-3 LAUNCH COSTS--NOMIN
Page 136 and 137: -115- Table A-5 LAUNCH COSTS FOR TH
Page 138 and 139: Table B-I POWER SYSTEM COMPARISONS
Page 140 and 141: -119- NOTES TO TABLE B-I (Cont.) mo
Page 142 and 143: -121- The duration of the data pass
Page 144 and 145: -123- INNNU AWA n -. s vo (I T 'API
Page 146 and 147: -125- each battery has its own char
Page 148 and 149: -127- Table B-2 POWER SUMMARY Chara
Page 150 and 151: -129- Appendix C COMMUNICATIONS AND
Page 152 and 153: -131- chiefly for storing commands
Page 154 and 155: -133- Table C-2 C&DH CHANGES REQUIR
Page 156 and 157: -135- Table C-3 C&DH CHANGES REQUIR
Page 158 and 159: -137- NOTES TO TABLE C-3 (Cont.) we
Page 160 and 161: - 139- Table D-1 ATTITUDE CONTROL A
Page 162 and 163: * -141- and three reaction wheels a
Page 164 and 165: -143- by the commonly adopted desig
Page 166 and 167: -145- Table E-l--Continued I Unit T
Page 168 and 169: -147- flight-proven elastomeric dia
Page 170 and 171: -149- Appendix F STRUCTURAL SUBSYST
Page 172 and 173: -151- points are provided by three
Page 174 and 175: -153- Table F-2 STPSS STRUCTURAL CO
Page 176 and 177: -155- Appendix G THERMAL CONTROL SU
Page 178 and 179: -157- sunlight. These surfaces incl
Page 180 and 181: -159- Appendix H PROGRAM OPTIONS FO
Page 182 and 183:
I 4 I IQ. w ~ w 01 " 1 I I I I 0 .c
Page 184 and 185:
-163- Table H-4 ORBIT 2: PAYLOAD AS
Page 186 and 187:
-165- c0 k- c" Q N 3- W 0 0 IT -- c
Page 188 and 189:
-167- Table 1-7 CASE I (A)a PROGRAM
Page 190 and 191:
-169- Table H-9 CASES I (K) AND V (
Page 192 and 193:
-171- Table H-11 CASE II(B) PROGRAM
Page 194 and 195:
-173- Table H-13 CASE 111(C) PROGRA
Page 196 and 197:
-175- Table H-15 CASE 111(M) PROGRA
Page 198 and 199:
-177- Table H-17 CASE IV(D) PROGRAM
Page 200 and 201:
-17 9- Table H-19 CASE IV(N) PROGRA
Page 202 and 203:
-181- Table Hi-21 CASE V (E) PROGRA
Page 204 and 205:
-183- Table H-23 CASE VI(F) PROGRAM
Page 206 and 207:
-185- Appendix J AIR FORCE AND NASA
Page 208 and 209:
MEMORANDUM OF AGRE1MENT ON THE PROC
Page 210 and 211:
-189- 2.2 DOD SPACE TEST PROGRAM: T
Page 212 and 213:
-191- l4.1.7 STP will review the HF
Page 214 and 215:
I -193- 5.0 NASA AND DOD FINANCIAL
Page 216 and 217:
-195- 5.4.3 Post Delivery Phase: NA
Page 218 and 219:
I '-197- $4 .0 0 A 0 f-4 ;C:ur 0 V
Page 220 and 221:
t 4 In I Io H 0p Ad ~t m 00 -199- E
Page 222 and 223:
-201- COPIED August 24, 1976 Honora
Page 224 and 225:
-204- 13. "The National Space Progr
Page 226 and 227:
-206- 39. Tec hnical vpoaal for a M
show all

A Case Study in NASA-DoD - The Black Vault

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?