Spacecraft material applications: Long-term stability questions
Abstract
An examination of the materials concerns for a variety of spacecraft components shows that long-term stability within the space environments is a major issue in the design of large space antenna systems. This survey paper will review some of the more recent work on the effect of space environment on (1) thin films, (2) structural composites, and (3) thermal control materials. Degradation in thermal-mechanical and optical properties associated with atmospheric and trapped particles and ultraviolet light will be highlighted. Finally, the dimensional instability associated with microcracking during thermal cycling will be examined and a methodology for estimating thermal fatigue effects from results of mechanical fatigue tests will be presented.
- Publication:
-
Large Space Antenna Systems Technology
- Pub Date:
- May 1983
- Bibcode:
- 1983lsas.rept..241C
- Keywords:
-
- Charged Particles;
- Composite Materials;
- Radiation Effects;
- Spacecraft Components;
- Spacecraft Construction Materials;
- Aerospace Environments;
- Microcracks;
- Polymers;
- Reaction Kinetics;
- Solar Flux;
- Thermal Cycling Tests;
- Thin Films;
- Trapped Particles;
- Ultraviolet Radiation;
- Launch Vehicles and Space Vehicles