- 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 132 and 133:
'I FI Table A-2 SPACECRAFT COSTS WI
- 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 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