Evaluation philosophy for shuttle launched payloadsSome 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.
Document ID
19760032843
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Heuser, R. E. (NASA Goddard Space Flight Center Greenbelt, Md., United States)