Deep Throttle of a Nitrous Oxide and Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor
Author:
Affiliation:
1. Mechanical and Aerospace Engineering Department, Utah State University, Logan, Utah 84322
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/10.2514/1.B34967
Reference26 articles.
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3. A Historical Systems Study of Liquid Rocket Engine Throttling Capabilities
4. BradleyM. “Space Shuttle Main Engine Off-Nominal Low Power Level Operation,” AIAA Paper 1997-2685, July 1997.
5. TRW pintle engine heritage and performance characteristics
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