This document provides performance properties on major spacecraft materials and subsystems that have been exposed to the low-Earth orbit (LEO) space environment. Spacecraft materials include metals, polymers, composites, white and black paints, thermal-control blankets, adhesives, and lubricants. Spacecraft subsystems include optical components, solar cells, and electronics. Information has been compiled from LEO short-term spaceflight experiments (e.g., space shuttle) and from retrieved satellites of longer mission durations (e.g., Long Duration Exposure Facility). Major space environment effects include atomic oxygen (AO), ultraviolet radiation, micrometeoroids and debris, contamination, and particle radiation. The main objective of this document is to provide a decision tool to designers for designing spacecraft and structures. This document identifies the space environments that will affect the performance of materials and components, e.g., thermal-optical property changes of paints due to UV exposures, AO-induced surface erosion of composites, dimensional changes due to thermal cycling, vacuum-induced moisture outgassing, and surface optical changes due to AO/UV exposures. Where appropriate, relationships between the space environment and the attendant material/system effects are identified. Part 2 covers thermal control systems, power systems, optical components, electronic systems, and applications.
Space Environmental Effects on Spacecraft: Leo Materials Selection Guide, Part 2
1995
412 pages
Report
Keine Angabe
Englisch
Unmanned Spacecraft , Manned Spacecraft , Materials Degradation & Fouling , Earth orbital environments , Low earth orbits , Optical equipment , Spacecraft construction materials , Spacecraft design , Spacecraft electronic equipment , Spacecraft power supplies , Thermal control coatings , Aluminum coatings , Charged particles , Electric batteries , Micrometeoroids , Mirrors , Optical filters , Oxygen atoms , Paints , Solar cells , Solar reflectors , Ultraviolet radiation