| 发明名称 |
LOW VELOCITY INJECTOR MANIFOLD FOR HYPERGOLIC ROCKET ENGINE |
| 摘要 |
A fuel manifold for a thrust chamber assembly includes a main fuel chamber which is generally frustro-conical in shape. The main fuel chamber provides a resonance frequency that is at least an order of magnitude lower than an acoustic resonance frequency of a combustion chamber.
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| 申请公布号 |
US2010037590(A1) |
申请公布日期 |
2010.02.18 |
| 申请号 |
US20080193679 |
申请日期 |
2008.08.18 |
| 申请人 |
BROWN WILLIAM S;WALCZUK THOMAS M;NOBLE RODNEY;DODD FREDERICK |
发明人 |
BROWN WILLIAM S.;WALCZUK THOMAS M.;NOBLE RODNEY;DODD FREDERICK |
| 分类号 |
F02K9/52 |
主分类号 |
F02K9/52 |
| 代理机构 |
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代理人 |
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