Numerical and experimental research on axial injection end-burning hybrid rocket motors with polyethylene fuel
Author:
Funder
National Natural Science Foundation of China
Academic Excellence Foundation of BUAA for PHD Students
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference32 articles.
1. Hybrid rocket propulsion technology for space transportation revisited - propellant solutions and challenges;Okninski;FirePhysChem,2021
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3. Numerical analysis on combustion characteristics of hybrid rocket motor with star-tube segmented grain;Li;Chin J Aeronaut,2023
4. Multi-disciplinary design optimization with fuzzy uncertainties and its application in hybrid rocket motor powered launch vehicle;Wang;Chin J Aeronaut,2020
5. Combustion characteristics of the end burning hybrid rockets in laminar flow;Matsuoka;Acta Astronaut,2011
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