Optimal Design and Control of Hybrid Rockets for Access to Space
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference21 articles.
1. 1Dornheim, M.A. "Reaching 100 km," Aviation Week & Space Technology, Vol.161, No. 6, Aug. 2004.
2. Combustion of Liquefying Hybrid Propellants: Part 1, General Theory
3. Application of a Genetic Algorithm to the Optimization of Hybrid Rockets
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