NASA/TP-1999-209260, Dooling, D. and Finckenor, M.M., Material Selection Guidelines to Limit Atomic Oxygen Effects on Spacecraft Surfaces , Prepared for NASA's Space Environments and Effects (SEE) Program*D2 Associates, 555 Sparkman Dr., Suite 820C, Huntsville, AL 35816, June 1999, pp. 44, Format(s): PDF 17094k |
Material Selection Guidelines to Limit Atomic Oxygen Effects on Spacecraft Surfaces provides guidelines in selecting materials for satellites and space platforms, designed to operate within the Low-Earth orbit environment, which limit the effects of atomic oxygen interactions with spacecraft surfaces. This document should be treated as an introduction rather than a comprehensive guide since analytical and flight technologies continue to evolve, flight experiments are conducted as primary or piggyback opportunities arise, and our understanding of materials interactions and protection methods grows. The reader is urged to consult recent literature and current web sites containing information about research and flight results.
| Keywords: | materials, space materials |
|---|---|
| Subjects: | Astronautics: Spacecraft Design, Testing And Performance |
| ID Code: | 481 |
| Deposited On: | 24 July 2002 |