发明名称 ARTIFICIAL SATELLITE
摘要 <P>PROBLEM TO BE SOLVED: To reduce a risk of intrusion control of contamination into a propellant tank concerning propellant filling at a launching site to an artificial satellite, and a cost required for propellant filling work. Ž<P>SOLUTION: The artificial satellite comprises a satellite structure, the propellant tank equipped with a connecting adaptor and a valve mechanism with an ammunition, a pipe detachably connecting the connecting adaptor of the propellant tank and a thruster, and an ammunition control device driving the valve mechanism with the ammunition. The propellant tank is installed in the artificial satellite at the launching site of the artificial satellite. Ž<P>COPYRIGHT: (C)2010,JPO&INPIT Ž
申请公布号 JP2009241805(A) 申请公布日期 2009.10.22
申请号 JP20080091968 申请日期 2008.03.31
申请人 MITSUBISHI ELECTRIC CORP 发明人 ARISAKA ICHITARO
分类号 B64G1/40 主分类号 B64G1/40
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