Reconstructed Ballistic Data Versus Wax Regression-Rate Intrusive Measurement in a Hybrid Rocket
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Sagamihara City, Kanagawa 252-5210, Japan
2. Politecnico di Milano, 20156 Milan, Italy
Funder
Japan Government
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference35 articles.
1. Progress in Astronautics and Aeronautics;Altman D.,2007
2. Low cost small-satellite access to space using hybrid rocket propulsion
3. Hybrid rocket propulsion systems for outer planet exploration missions
4. Optimal Robust Design of Hybrid Rocket Engines
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