发明名称 THRUSTER USING NITROUS OXIDE
摘要 A thruster is provided that makes it possible to reduce and eventually eliminate the toxicity of storable liquid propellant and improve the low-temperature environment adaptability of propulsion system using the storable liquid propellant. The thruster produces thrust by using catalytic decomposition gas obtained by catalytically decomposing nitrous oxide with a nitrous oxide decomposition catalyst.
申请公布号 US2009007541(A1) 申请公布日期 2009.01.08
申请号 US20070951298 申请日期 2007.12.05
申请人 JAPAN AEROSPACE EXPLORATION AGENCY;SHOWA DENKO K.K. 发明人 KAWAGUCHI JUNICHIRO;TOKUDOME SHINICHIRO;HABU HIROTO;YAGISHITA TSUYOSHI;HOTTA MASATOSHI
分类号 C06D5/00 主分类号 C06D5/00
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