Particle simulations of helium microthruster flows
Author:
Affiliation:
1. Eloret Institute, Palo Alto, California 94303
2. Stanford University, Stanford, California 94305
3. Lockheed Missiles and Space Company, Sunnyvale, California 94089
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26433
Reference17 articles.
1. Rocket nozzle lip flow by direct simulation Monte Carlo method
2. Assessment of Impingement Effects in the Isentropic Core of a Small Satellite Control Thruster Plume
3. Experimental and numerical investigations of low-density nozzle and plume flows of nitrogen
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