发明名称 AEROSPACE VEHICLE SEPARATOR
摘要 PROBLEM TO BE SOLVED: To solve the problem that a separated space satellite can not keep the predetermined attitude because the separation force, can not be uniformly applied to the space satellite because of the time difference at the start of the operation of the separation springs, as an electric separation bolt is operated, then a clamp band is disengaged after the electric separation bolt is cut, and the separation spring of the disengaged part is operated in the conventional aerospace vehicle separator. SOLUTION: An instantaneous gas generation driving force generator is mounted as the separation releasing force for separation springs, whereby the gas is generated after the force of constraint by a clamp band or the like is sufficiently excluded, and the separation force is generated as the driving force.
申请公布号 JP2001106199(A) 申请公布日期 2001.04.17
申请号 JP19990287903 申请日期 1999.10.08
申请人 MITSUBISHI ELECTRIC CORP 发明人 ISHII TOYOHIKO
分类号 B64G1/64;(IPC1-7):B64G1/64 主分类号 B64G1/64
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