Space Shuttle Orbiter molecular environment induced by the supplemental flash evaporator system
Author:
Affiliation:
1. NASA Johnson Space Center, Houston, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25816
Reference10 articles.
1. Space Shuttle contamination measurements from flights STS-1 through STS-4
2. An analysis of return flux from the Space Shuttle Orbiter RCS engines
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1. The interaction of the atmosphere with the space shuttle thruster plume: The NH(A-X) 336-nm emission;Journal of Geophysical Research: Space Physics;1996-03-01
2. Optical emissions from the interaction of the Space Shuttle with the atmosphere - The NH(A-X) 336 nm emission;33rd Aerospace Sciences Meeting and Exhibit;1995-01-09
3. O(1S) 557.7 nm and O(1D) 630 nm emissions in shuttle thruster plumes;Journal of Geophysical Research;1995
4. Methylhydrazine Reactions with O+ and Other Ions at Hyperthermal Collision Energies;The Journal of Physical Chemistry;1994-11
5. Reactions of hydrazine with atomic oxygen(1+) and other ions at suprathermal energies;The Journal of Physical Chemistry;1992-05
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