Ignition Characteristics of GH2/GOx Mixture Using Laser Ablation Ignition

Author:

Mori Koichi,Kusaka Kazuo,Fujita Kazuhisa,Niino Masayuki,Kmetik Viliam,Nakano Masakatsu,Takahashi Hideaki,Nakajima Shoji,Arakawa Yoshihiro

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Reference11 articles.

1. 1) Kimura, I.: Rocket Engineering, Yokendo, Tokyo, 1993. (in Japanese)

2. 2) Sutton, G. P.: Rocket Propulsion Elements, John Wiley & Sons, New York, 1992.

3. 3) Kmetik, V., Kumagai, T., Kusaka, K., Kisara, K., Kuroda, Y., Niino, M. and Imasaki, K.: Laser Ignition of Fluid Propellants for RCS, ISTS 2000-a-25, 2000.

4. 4) Nakajima, S., Mishima, H., Kuroda, M., Hashimoto, Y. and Shimoda, M.: Investigation on the Basic Technologies for Non-Toxic RCS, Symposium on Space Transportation, ISAS, Kanagawa, 1999.

5. 5) Institute of the Electrical Engineers of Japan: Laser Ablation and Its Application, Corona Inc., Tokyo, 1999. (in Japanese)

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