A Case Study in NASA-DoD - The Black Vault

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Table H-4
ORBIT 2:
PAYLOAD ASSIGNMENTS
Orbit 2:
Elliptical (7,000 x 200 n mi), polar
Payload number .1 6 1.1 .12 13 14 17 21 22 3.1 32 46 50
Weight (lb) 17 16 4 815s 8 4 44 70 1.8 1 5 110
Candidate Spacecraft
AEN y y y y y y y y y Y Y
STPSS-S x x
STPSS-LC x x x x x x x x x x x x x
STPSS-P or MM~S Ix x x x X I x x x x x x x A.
Table H1-5
ORBITS 3, 4, 5, 6, 7, and 3:
PAYLOAD ASSIGNMENTS
Orbit 3a 4b 5c 6d 7" 8f
Payload number 3 16 44 52 2 24 7 10 43 8 25 30I
Weight (lb) 12 3 147 13 29 2 125 19 475 (30) 43 30
Candidate Spacecraft
AEN Y Y y y y Y y y y
STPSS-S x x x x
STPSS-LC x x x x x x x x x x
STPSS-P or MMS x x x K x x K x x I K K
aGeosynchronous (19,372 n mi) circular, low inclination, sun-oriented.
b,00n mi circular, low inclination.
C12-hour orhit, 21,000 x 900 n mi, 63.4 deg inclination.
dGeosynchronous circular, low inclination, earth-oriented.
e 3 ,200 x 150 n mi, 30 deg inclination.
I ~f180 n iii circular, polar.