Development and Testing of a Lab-scale Test-bench for Hybrid Rocket Engines
Author:
Affiliation:
1. Royal Military Academy
2. Université Libre de Bruxelles
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-2722
Reference23 articles.
1. Overview on hybrid propulsion
2. Hybrid Rockets with Axial Injector: Port Diameter Effect on Fuel Regression Rate
3. TOSON, Elena et KARABEYOGLU, Arif M. Design and Optimization of Hybrid Propulsion Systems for In-Space Application. In: 51st AIAA/SAE/ASEE Joint Propulsion Conference. 2015. p.3937.
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