Studies on the effects of the interplanetary space environment on thermal-control coatings.
Author:
Affiliation:
1. Lockheed Missiles & Space Company, Polo Alto, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4263
Reference24 articles.
1. Effects of electron bombardment on the optical properties of spacecraft temperature control coatings.
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1. Ion Flux Environments in Interplanetary Space;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
2. RESULTS FROM THE ATS-3 REFLECTOMETER EXPERIMENT;Thermophysics: Applications to Thermal Design of Spacecraft;1970
3. Heat transfer—a review of current literature;International Journal of Heat and Mass Transfer;1968-10
4. Optical solar reflector - A highly stable, low alpha sub S/epsilon spacecraft thermal control surface.;Journal of Spacecraft and Rockets;1968-09
5. Comment on "Effect of Simulated Micrometeoroid Exposure on Performance of NIP Silicon Solar Cells";AIAA Journal;1968-02
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