Autoignitable and Restartable Hybrid Rockets Using Catalytic Decomposition of an Oxidizer
Author:
Affiliation:
1. Aerospace Engineering, Korea Advanced Institute of Science and Technology, Daejeon 305-701, Republic of Korea
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.B34739
Reference8 articles.
1. Nitrous oxide as a rocket propellant
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5. Scale-Up Tests of High Regression Rate Paraffin-Based Hybrid Rocket Fuels
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