发明名称 SATELLITE RELEASE DEVICE
摘要 PROBLEM TO BE SOLVED: To make it easy to maintain a correct release posture without damaging a spinning satellite. SOLUTION: This device is provided with an inner cylinder 11 on which spiral grooves M, N are formed on a surface thereof and which is coupled to a satellite to be released, an outer cylinder 12 concentric with the inner cylinder 11 and which has a diameter different from that of the inner cylinder 11, a constant tension winding mechanism 16 mounted on the outer cylinder 12 for rotating the inner cylinder 11, and a guide roller R that rotates along the groove N and which makes the inner cylinder 11 move in a helicoidal motion.
申请公布号 JP2000309300(A) 申请公布日期 2000.11.07
申请号 JP19990117980 申请日期 1999.04.26
申请人 TOSHIBA CORP 发明人 SATO TAKAYUKI;TSUKAJIMA TAKASHI
分类号 B64G1/64;(IPC1-7):B64G1/64 主分类号 B64G1/64
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