Experimental Studies of Protrusion-Inserted Hybrid Rocket Motor with Varying L/D Ratio
Author:
Affiliation:
1. Birla Institute of Technology, Mesra, Ranchi 835 215, India
Funder
Science and Engineering Research Board, Department of Science and Technology, Government of India.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference29 articles.
1. Progress in Astronautics and Aeronautics;Altman D.,2006
2. Approaches to Low Fuel Regression Rate in Hybrid Rocket Engines
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