发明名称 |
ROCKET ENGINE |
摘要 |
The invention concerns a rocket engine wherein the combustion chamber consists of at least one first monolithic component made of a thermostructural composite material comprising a porous wall (5) through which the fuel is introduced in the core (C) of said combustion chamber. A small part of said fuel is directed towards the neck (3) for it to be cooled.
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申请公布号 |
WO03074859(A1) |
申请公布日期 |
2003.09.12 |
申请号 |
WO2003FR00630 |
申请日期 |
2003.02.27 |
申请人 |
EADS SPACE TRANSPORTATION SA;MBDA FRANCE;CALABRO, MAX |
发明人 |
CALABRO, MAX |
分类号 |
F02K9/00;F02K9/52;F02K9/64;F02K9/97;(IPC1-7):F02K9/64 |
主分类号 |
F02K9/00 |
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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