The structural design, analysis, and mechanical integration of the synchronous meteorological satellite system are presented. The subjects discussed are: (1) spacecraft configuration, (2) structural design, (3) static load tests, (4) fixed base sinusoidal vibration survey, (5) flight configuration sinusoidal vibration tests, (6) spacecraft acoustic test, and (7) separation and shock test. Descriptions of the auxiliary propulsion subsystem, the apogee boost motor, communications system, and thermal control subsystem are included.
Synchronous meteorological satellite system description document, volume 3
1971-12-01
Report
Keine Angabe
Englisch
The Synchronous Meteorological Satellite /SMS/ system
NTRS | 1973
|Synchronous meteorological satellite spin testing
NTRS | 1975
|