A method to define low-altitude rocket exhaust characteristics and impingement effects
Author:
Affiliation:
1. General Dynamics, Pomona, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29961
Reference18 articles.
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3. Numerical simulation and field testing of flame-jet thermal spallation drilling—1. Model development;International Journal of Heat and Mass Transfer;1991-03
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5. Aluminized propellants and a method defining low-altitude exhaust plumes;Journal of Spacecraft and Rockets;1986-03
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