| 发明名称 |
ROCKET ENGINE MEMBER AND METHOD FOR MANUFACTURING A ROCKET ENGINE MEMBER |
| 摘要 |
The invention relates to a liquid fuel rocket engine member (10). The member has a load bearing wall structure (14) comprising a plurality of cooling channels (11). For improving the heat transfer, a material with a higher thermal conductivity than the load bearing wall structure (14) has been applied to the wall structure. |
| 申请公布号 |
WO02055862(A1) |
申请公布日期 |
2002.07.18 |
| 申请号 |
WO2002SE00025 |
申请日期 |
2002.01.09 |
| 申请人 |
VOLVO AERO CORPORATION;HAEGGANDER, JAN;BOMAN, ARNE |
发明人 |
HAEGGANDER, JAN;BOMAN, ARNE |
| 分类号 |
F02K1/00;B22F3/105;F02K9/64;F02K9/97;(IPC1-7):F02K9/64 |
主分类号 |
F02K1/00 |
| 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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