Thrust Modulation in a Nitrous Oxide/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor-Reference-Cited by-同舟云学术

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Thrust Modulation in a Nitrous Oxide/Hydroxyl-Terminated Polybutadiene Hybrid Rocket Motor

Published:2006-07-09 Issue: Volume: Page:
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Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Rajesh Kannalath Krishnan

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. 1Krishnan, S. "Hybrid Rocket Technology: An Overview," Third International High Energy Materials Conference and Exhibit, Thiruvanthapuram, India, Dec.6-8, 2000, pp.62-71.

2. Fuel Regression Rate in Hydroxyl-Terminated-Polybutadiene/Gaseous-Oxygen Hybrid Rocket Motors

3. Combustion Experiments in Hydrogen Peroxide/Polyethylene Hybrid Rocket with Catalytic Ignition

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