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 |
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代理人 |
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主权项 |
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地址 |
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