Dynamic Modeling of Hybrid Rocket Combustion
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5464
Reference18 articles.
1. Karabeyoglu, M. A. “Transient Combustion in Hybrid Rockets,” Ph.D. Dissertation,Dept. of Aeronautics and Astronautics, Stanford Univ., Stanford, CA,Aug. 1998.
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