发明名称 |
PAYLOAD LAUNCHING SYSTEM |
摘要 |
<p num="1"><br/><br/><br/>This invention relates to a system for launching a payload. A rotating <br/>flywheel (11) accelerates a traditionally designed rocket (16) to a <br/>significant speed. Rotational energy from the flywheel (11) is transferred in <br/>the form of kinetic energy through a spiral surface and a cable (14) to the <br/>rocket (16). The system comprises a smaller rocket (16) carrying less fuel, <br/>provided with a smaller first stage engine. All other components of the system <br/>are re-used. This leads to a simpler and more efficient design of the rocket <br/>(16) and to a considerable reduction in launch costs.<br/>
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申请公布号 |
CA2544236(A1) |
申请公布日期 |
2005.06.02 |
申请号 |
CA20042544236 |
申请日期 |
2004.10.31 |
申请人 |
DEMOLE, FREDERIC, JEAN-PIERRE |
发明人 |
DEMOLE, FREDERIC JEAN-PIERRE |
分类号 |
B64G5/00;B64G1/00;F41B15/00;F41F3/04 |
主分类号 |
B64G5/00 |
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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