Optimization of Hybrid Rocket Engines for Small Satellite Launchers
Author:
Affiliation:
1. Technical University of Turin
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4926
Reference16 articles.
1. Optimal Design of Hybrid Rocket Motors for Launchers Upper Stages
2. Optimization of Hybrid Upper-Stage Motor with Coupled Evolutionary/Indirect Procedure
3. Approximate and Exact Approaches for the Optimization of Hybrid-Rocket Upper Stage
4. Optimal Design and Control of Hybrid Rockets for Access to Space
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