LAUNCHING A FLIGHT VEHICLE
| 专利类型 | 发明申请 | 法律事件 | |
| 专利有效性 | 公开 | 当前状态 | |
| 申请号 | PCT/IB2007052827 | 申请日 | 2007-07-16 |
| 公开(公告)号 | WO2008010180A3 | 公开(公告)日 | 2008-03-06 |
| 申请人 | SPACEGO TECHNOLOGIES PROPRIETA; LEUSCHNER ANDRIES HERMANN; | 申请人类型 | 其他 |
| 发明人 | LEUSCHNER ANDRIES HERMANN; | 第一发明人 | LEUSCHNER ANDRIES HERMANN |
| 权利人 | SPACEGO TECHNOLOGIES PROPRIETA,LEUSCHNER ANDRIES HERMANN | 权利人类型 | 其他 |
| 当前权利人 | SPACEGO TECHNOLOGIES PROPRIETA,LEUSCHNER ANDRIES HERMANN | 当前权利人类型 | 其他 |
| 省份 | 当前专利权人所在省份： | 城市 | 当前专利权人所在城市： |
| 具体地址 | 当前专利权人所在详细地址： | 邮编 | 当前专利权人邮编： |
| 主IPC国际分类 | F41F3/073 | 所有IPC国际分类 | F41F3/073 ; F41B6/00 |
| 专利引用数量 | 7 | 专利被引用数量 | 0 |
| 专利权利要求数量 | 0 | 专利文献类型 | A3 |
| 专利代理机构 | 专利代理人 | ||
| 摘要 | This invention relates to launching of a flight vehicle, such as a rocket, an aircraft and the like, from a generally upwardly directed subterranean launch shaft of at least 300 m length, preferably of a length of 500 m or more. Preferably, the launch shaft is an amortized mine shaft. Launching is by means of one of, or a combination of, several possible propulsion systems. For each system, at least some components are external of the flight vehicle and associated with or mounted in the launch shaft. One kind of propulsion system may use expansion of gas in the launch shaft behind the flight vehicle. Other propulsion systems use electromagnetism or Lorentz-type actuators, such as a coil gun or gauss gun, a linear induction motor or linear synchronous motor, or a rail gun. The launch shaft mounts guiding means for guiding the flight vehicle along the launch shaft. | ||
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