发明名称 |
PAYLOAD LAUNCHING SYSTEM |
摘要 |
This invention relates to a system for launching a payload. A rotating flywheel (11) accelerates a traditionally designed rocket (16) to a significant speed. Rotational energy from the flywheel (11) is transferred in the form of kinetic energy through a spiral surface and a cable (14) to the rocket (16). The system comprises a smaller rocket (16) carrying less fuel, provided with a smaller first stage engine. All other components of the system are re-used. This leads to a simpler and more efficient design of the rocket (16) and to a considerable reduction in launch costs. |
申请公布号 |
EA008152(B1) |
申请公布日期 |
2007.04.27 |
申请号 |
EA20060000870 |
申请日期 |
2004.10.31 |
申请人 |
DEMOLE FREDERIC, JEAN-PIERRE |
发明人 |
DEMOLE FREDERIC, JEAN-PIERRE |
分类号 |
B64G1/00;B64G5/00;F41B15/00;F41F3/04 |
主分类号 |
B64G1/00 |
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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