发明名称 LAUNCHING AZIMUTH CONTROL DEVICE OF AIR-LAUNCHING SYSTEM
摘要 PROBLEM TO BE SOLVED: To provide a launching azimuth control device of an air-launching system, which can keep an azimuth of a rocket as a preset azimuth without being affected by an air current during descent.SOLUTION: A launching azimuth control device includes: a hollow body 22 that is suspended by a parachute 13 and suspends front and rear sections of a platform 12 by connecting harnesses 16a and 16b, during descent; a fly wheel 24 that is provided in the hollow body 22 and that rotates on a vertical axis 25 during the descent; and an azimuth controller 26 that controls the rotational speed and rotational direction of the fly wheel 24.
申请公布号 JP2014091413(A) 申请公布日期 2014.05.19
申请号 JP20120242960 申请日期 2012.11.02
申请人 IHI AEROSPACE CO LTD 发明人 YOKOTE ATSUSHI;KIMURA SATOHIDE;NOGUCHI YUICHI
分类号 B64D17/34;B64D7/08;B64G1/28 主分类号 B64D17/34
代理机构 代理人
主权项
地址
您可能感兴趣的专利