| 发明名称 |
ROCKET PROPELLED PAYLOAD WITH DIVERT CONTROL SYSTEM WITHIN NOSE CONE |
| 摘要 |
A rocket is provided and includes booster stages at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction and a divert control system housed entirely in the nose cone for controlling an orientation of the propulsion direction. |
| 申请公布号 |
EP2917683(A4) |
申请公布日期 |
2016.07.27 |
| 申请号 |
EP20130853167 |
申请日期 |
2013.09.03 |
| 申请人 |
RAYTHEON COMPANY |
发明人 |
FACCIANO, ANDREW B.;ALKEMA, MICHAEL S.;MOORE, ROBERT T. |
| 分类号 |
F42B15/01 |
主分类号 |
F42B15/01 |
| 代理机构 |
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代理人 |
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| 主权项 |
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