The goal of the space flight program at the Center for Commercial Development of Space (CCDS)--Materials for Space Structures is to provide environmentally stable structural materials to support the continued humanization and commercialization of the space frontier. Information on environmental stability will be obtained through space exposure, evaluation, documentation, and subsequent return to the supplier of the candidate material for internal investigation. This program provides engineering and scientific service to space systems development firms and also exposes CCDS development candidate materials to space environments representative of in-flight conditions. The maintenance of a technological edge in space for NASA suggests the immediate search for space materials that maintain their structural integrity and remain environmentally stable. The materials being considered for long-lived space structures are complex, high strength/weight ratio composites. In order for these new candidate materials to qualify for use in space structures, they must undergo strenuous testing to determine their reliability and stability when subjected to the space environment. Ultraviolet radiation, atomic oxygen, debris/micrometeoroids, charged particles radiation, and thermal fatigue all influence the design of space structural materials. The investigation of these environmental interactions is the key purpose of this center. Some of the topics discussed with respect to the above information include: the Space Transportation System, mission planning, spaceborne experiments, and space flight payloads.
Transition of Ground-Based Space Environmental Effects Testing to the Space Environment
1991
7 pages
Report
No indication
English
Unmanned Spacecraft , Manned Spacecraft , Spacecraft construction materials , Structural stability , Aerospace environments , Environmental tests , Mission planning , Space commercialization , Space transportation system , Spaceborne experiments , Spacecraft structures , Charged particles , Corrosion tests , Oxidation resistance , Oxygen atoms , Space shuttle payloads , Space stations , Structural failure , Thermal fatigue , Ultraviolet radiation
Ground Testing and Simulation of Space Environment Hazards
British Library Conference Proceedings | 1995
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