| 发明名称 |
ORIENTABLE ROCKET-MOTOR SYSTEM |
| 摘要 |
A system allowing for the tilting of the rocket motor such that, in the tilted position, the centre of the nozzle is located at least approximately on the neutral orientation axis of said rocket motor. |
| 申请公布号 |
SG11201508609R(A) |
申请公布日期 |
2015.11.27 |
| 申请号 |
SG11201508609R |
申请日期 |
2014.04.22 |
| 申请人 |
AIRBUS DEFENCE AND SPACE SAS |
发明人 |
RUFFINO FABRICE;FAURE BENJAMIN |
| 分类号 |
F02K9/80;F02K9/56;F02K9/84 |
主分类号 |
F02K9/80 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
|
| 地址 |
|
