Current status of rocket developments in universities -development of a small hybrid rocket with a swirling oxidizer flow type engine

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Yuasa, Saburo; Kitagawa, Koki;
(2005)

To develop an experimental small hybrid rocket with a swirling gaseous oxygen flow type engine, we made a flight model engine. Burning tests of the engine showed that a maximum thrust of 692 N and a specific impulse of 263 s (at sea level) were achieved. We designed a s... View more
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