Affiliation:
1. NASA Ames Research Center
2. Stanford University
Publisher
American Institute of Aeronautics and Astronautics
Reference13 articles.
1. Combustion of Liquefying Hybrid Propellants: Part 1, General Theory
2. Guthrie,D.M.andWolf,R.S.(1991)Non-acoustic combustion instability in hybrid rocket motors. AMROCCo. N 91-24250.
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