Combustion and Regenerative Cooling Characteristics of LOX/Methane Engine

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概要

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• The regenerative cooled LOX/methane engine is considered by the cooperative research with JAXA, MHI, and IHI. As a part of this cooperation, the experiments and analysis about LOX/methane combustion instability and regenerative cooling characteristics were carried out because the lack of the fundamental LOX/methane properties was identified as a risk through engine design, production, test, and operation.

著者

• KAWASHIMA Hideto

  Japan Aerospace Exploration Agency (JAXA)

• OKITA Koichi

  Japan Aerospace Exploration Agency (JAXA)

• AOKI Kenji

  Japan Aerospace Exploration Agency (JAXA)

• AZUMA Nobuyuki

  Japan Aerospace Exploration Agency (JAXA)

• KUMAKAWA Akinaga

  Japan Aerospace Exploration Agency (JAXA)

• ONODERA Takuo

  Japan Aerospace Exploration Agency (JAXA)

• YOSHIDA Seiji

  Japan Aerospace Exploration Agency (JAXA)

• NEGISHI Hideyo

  Japan Aerospace Exploration Agency (JAXA)

• MANAKO Hiroyasu

  Mitsubishi Heavy Industry (MHI)

• KOGANEZAWA Takashi

  Mitsubishi Heavy Industry (MHI)

関連論文

• Combustion and Regenerative Cooling Characteristics of LOX/Methane Engine
• Preparation and Properties of Disilane and Disiloxane Unit-Fused Poly(diphenylamine)

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