Experimental Study of a Hypergolically Ignited Liquid Bipropellant Rotating Detonation Rocket Engine
Author:
Affiliation:
1. Purdue University, West Lafayette, Indiana 47907
2. Air Force Institute of Technology, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Reference12 articles.
1. Continuous Spin Detonations
2. Experimental research on rotating detonation with liquid hypergolic propellants
3. An experimental description of destructive liquid rocket resonant combustion.
4. Response of a Liquid Jet in a Multiple-Detonation Driven Crossflow
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