Experimental and Numerical Investigation of Throttling Response Mechanisms in Axial-Injection End-Burning Hybrid Rockets
Author:
Affiliation:
1. Hokkaido University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-3500
Reference10 articles.
1. Verification Firings of End-Burning Type Hybrid Rockets
2. Investigation of axial-injection end-burning hybrid rocket motor regression
3. Y. Okutani, Y. Saito, M. Kimino, A. Tuji, K. Soeda, H. Nagata, Investigation of Regression Rate under High-Pressure in Axial-Injection End-Burning Hybrid Rockets, in:2018 Joint Propulsion Conference, American Institute of Aeronautics and Astronautics, Reston, Virginia, 2018. https://doi.org/10.2514/6.2018-4529.
4. Investigation of Throttling Response Characteristics of Axial-Injection End-Burning Hybrid Rockets
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