The Status of the Research and Development of LNG Rocket Engines in Japan

Author:

Asakawa Hiroya,Nanri Hideaki,Aoki Kenji,Kubota Isao,Mori Hatsuo,Ishikawa Yasuhiro,Kimoto Kenichi,Ishihara Shinji,Ishizaki Shinichiro

Publisher

Springer International Publishing

Reference21 articles.

1. Masahiro I et al (2010) Full duration firing test results of 100 kN LOx/LNG engine. In: Paper presented at the Space Propulsion 2010, San Sebastian, 3–6 May 2010

2. Kubota I et al (2012) Current development status of LNG propulsion system. In: Paper presented at the 53th conference on aerospace propulsion and power, Geibunkan, 4–5 Mar 2012

3. Kano Y et al (2012) Overview of LNG propulsion system development. In: Paper presented at the 63rd international astronautical congress, Naples, 1–5 Oct 2012

4. Taya K et al (2013) Development and test of the LOx/LNG regenerative cooled rocket engine (2nd report). In: Paper presented at the 29th international symposium on space technology and science, Nagoya congress center, Nagoya, 2–9 June 2013

5. Taya K et al (2014) Development and test of the LOx/Methane regenerative cooled rocket engine. In: Paper presented at space propulsion 2014, Cologne, 19–22 May 2014

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