Scaling Parameters of Swirling Oxidizer Injection in Hybrid Rocket Motors
Author:
Affiliation:
1. University of Padua, 35131 Padua, Italy
2. Stanford University, Sunnyvale, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B36241
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1. Cost and performance payoffs inherent in increased fuel regression rates
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5. Solid-Fuel Regression Rate Behavior of Vortex Hybrid Rocket Engines
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