发明名称 LOW-TOXICITY PROPELLANT
摘要 PROBLEM TO BE SOLVED: To provide a low-toxicity propellant of low toxicity used for boosters, such as thrusters and rockets, for posture control of artificial satellites. SOLUTION: The low-toxicity propellant is composed of main fuel for creating actuation gas for propulsion of the rockets etc., and an oxidizing agent, in which the oxidizing agent is hydrogen peroxide water and contains a complex or a metal salt or their mixture as a combustion assistant to assist combustion. COPYRIGHT: (C)2004,JPO
申请公布号 JP2004075497(A) 申请公布日期 2004.03.11
申请号 JP20020241478 申请日期 2002.08.22
申请人 MITSUBISHI HEAVY IND LTD 发明人 YASUTAKE AKINORI;TATEISHI MASAKAZU;TOMONAGA NARIYUKI;NOZAKI AKIHIRO;NISHIDA MITSURU;TSUTAYA HIROYUKI;MORIAI HIDEKI
分类号 C06D5/00;C06B23/00;C06B43/00;(IPC1-7):C06D5/00 主分类号 C06D5/00
代理机构 代理人
主权项
地址