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Dynamic tow maneuver orbital launch technique

机译:动态拖曳机动轨道发射技术

摘要

An orbital launch system and its method of operation use a maneuver to improve the launch condition of a booster rocket and payload. A towed launch aircraft, to which the booster rocket is mounted, is towed to a predetermined elevation and airspeed. The towed launch aircraft begins the maneuver by increasing its lift, thereby increasing the flight path angle, which increases the tension on the towline connecting the towed launch aircraft to a towing aircraft. The increased tension accelerates the towed launch aircraft and booster rocket, while decreasing the speed (and thus the kinetic energy) of the towing aircraft, while increasing kinetic energy of the towed launch aircraft and booster rocket by transferring energy from the towing aircraft. The potential energy of the towed launch aircraft and booster rocket is also increased, due to the increased lift. The booster rocket is released and ignited, completing the launch.
机译:轨道发射系统及其操作方法利用机动来改善助推火箭和有效载荷的发射条件。装有助推火箭的拖曳式飞行飞机被拖至预定的高度和空速。被牵引的发射飞机通过增加其升力开始机动,从而增加飞行路径角度,这增加了将被牵引的发射飞机连接到牵引飞机的牵引线上的张力。增大的张力使被牵引的发射飞机和助推火箭加速,同时降低了牵引飞机的速度(从而减小了动能),同时通过从牵引飞机传递能量来增加了被牵引的发射飞机和助推火箭的动能。由于升力的增加,被牵引的发射飞机和助推火箭的势能也增加了。助推火箭被释放并点燃,完成了发射。

著录项

  • 公开/公告号US8727264B1

    专利类型

  • 公开/公告日2014-05-20

    原文格式PDF

  • 申请/专利权人 ELBERT L. RUTAN;

    申请/专利号US201313914744

  • 发明设计人 ELBERT L. RUTAN;

    申请日2013-06-11

  • 分类号B64D3;B64C31/02;B64G1;

  • 国家 US

  • 入库时间 2022-08-21 16:04:28

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