Some approaches to space-shuttle payload evaluation are examined. Issues considered include subsystem replacement in low-cost modular spacecraft (LCMS), validation of spacelab payloads, the use of standard components in shuttle-era spacecraft, effects of shuttle-induced environments on payloads, and crew safety. The LCMS is described, and goals are discussed for its evaluation program. Concepts regarding how the evaluation should proceed are considered.
Evaluation philosophy for shuttle launched payloads
Aerospace Testing Seminar
1975-01-01
Miscellaneous
No indication
English
Evaluation philosophy for shuttle launched payloads
NTRS | 1975
|NTRS | 1977
|Communication with Shuttle payloads
Tema Archive | 1978
|Development of shuttle payloads
NTRS | 1977
|Shuttle entry technology payloads
NTRS | 1975
|