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Throttling capability and LOX vaporization for hybrid rocket engine with multi-section swirl injection method
Throttling capability and LOX vaporization for hybrid rocket engine with multi-section swirl injection method
2017
Shigeru Aso
Yasuhiro Tani
Masato Yamashita
Kazuya Komori
Tomohiro Yamasaki
Shohei Saiga
Ryohei Arakawa
Toru Shimada
Keywords:
Control engineering
Vaporization
Rocket engine
Bandwidth throttling
Materials science
Aerospace engineering
Correction
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