Solid propellant ignition motors for LH_2/LOX rocket engine system

Research Japanese OPEN
ARAKI, Tetsuo; AKIBA, Ryojiro; HASHIMOTO, Yasunari; AIHARA, Kenji; TOMITA, Etsu; YASUDA, Seiichi; 荒木, 哲夫; 秋葉, 鐐二郎; 橋本, 保成; 相原, 賢二; 富田, 悦; 安田, 誠一;
(1983)
  • Publisher: 宇宙科学研究所
  • Journal: 宇宙科学研究所報告:特集,volume 6,pages259-267 (issn: 0285-9920)
  • Subject:
    arxiv: Quantitative Biology::Subcellular Processes | Physics::Plasma Physics | Physics::Chemical Physics

Solid propellant ignition motors are used in the series of experiments of the 10 ton LH_2/LOX engine featured by the channel wall thrust chamber, This paper presents design specification, experiments and results obtained by actual applications of those ignition motors.
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