| 发明名称 |
THRUSTER COMPRISING A PLURALITY OF ROCKET MOTORS |
| 摘要 |
<p>The jet (40) has an air-fuel combustion chamber (42) and a plurality of rocket engines (11) arranged upstream from the combustion chamber (42), each rocket engine having its own combustion chamber with the wall thereof being cooled by lateral injection of fuel through said wall.</p> |
| 申请公布号 |
EP2313635(B1) |
申请公布日期 |
2014.04.16 |
| 申请号 |
EP20090784511 |
申请日期 |
2009.07.10 |
| 申请人 |
SNECMA |
发明人 |
CONRARDY, JEAN-MARIE;PEYRISSE, DANIEL |
| 分类号 |
F02K9/60;F02K7/18;F02K9/64 |
主分类号 |
F02K9/60 |
| 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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