Attitude-control rocket exhaust plume effects on spacecraft functional surfaces
Author:
Affiliation:
1. Space Division of North American Rockwell, Downey, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29861
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1. HYPERGOLIC IGNITION AT REDUCED PRESSURES
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3. Processes during the Hypergolic Ignition between Monomethylhydrazine (MMH) and Dinitrogen Tetroxide (N2O4) in Rocket Engines;Propellants, Explosives, Pyrotechnics;2005-02
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5. Contamination and space environmental effects on solar cells and thermal control surfaces;Journal of Spacecraft and Rockets;1995-09
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