Characterization of PolyMethylMethAcrylate as a Fuel for Hybrid Rocket Motors
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4530
Reference10 articles.
1. Advanced hybrid rocket motor experiments
2. Design of a Hybrid CubeSat Orbit Insertion Motor
3. Development Testing of Hybrid Rocket Motors Using Classical Fuels for Interplanetary CubeSats
4. Design of Interplanetary Hybrid CubeSat and SmallSat Propulsion Systems
5. Reconstruction Technique for Reducing Hybrid-Rocket Combustion Test Data
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