Issues Related to the Measurement of Regression Rate of Fast-Burning Hybrid Fuels
Author:
Affiliation:
1. Aerospace Engineering Department, Indian Institute of Technology Madras, Chennai 600 036, India
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.B34757
Reference38 articles.
1. Influence of a Conical Axial Injector on Hybrid Rocket Performance
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3. EvensB.BoyersE.KuoK.RishaG.ChiaveriniM. J. “Hybrid Rocket Investigation at Penn State University’s High Pressure Combustion Laboratory: Overview and Recent Results,” AIAA Paper 2009-5349, Aug. 2009.
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