What is it about?
An axial-injection end-burning hybrid rocket is a promising unconventional hybrid rocket that overcomes the disadvantages of the usual hybrid rockets. Past studies mainly focused on the combustion mechanism of gaseous oxidizers. We conduct firing tests using liquid oxygen as an oxidizer and study its fuel regression characteristics.
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This page is a summary of: Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets Using LOX, Journal of Propulsion and Power, September 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.b39819.
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