| 发明名称 |
ROCKET NOSE CONE |
| 摘要 |
rocketry. SUBSTANCE: spin-stabilized rocket nose has a nose fairing with a dropping device and a multiple parachute system with shroud lines attached to the rocket. The parachute canopies packed in separate sleeves are located in the nose fairing with a shift relative to the rocket spin axis. EFFECT: enhanced reliability of actuation of rocket parachute system. 3 cl, 1 dwg
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| 申请公布号 |
RU2151363(C1) |
申请公布日期 |
2000.06.20 |
| 申请号 |
RU19990102746 |
申请日期 |
1999.02.08 |
| 申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVOD;N PROIZV AOOT |
发明人 |
SOKOLOVSKIJ M.I.;BONDARENKO S.A.;ZYKOV G.A.;SHEIN A.G. |
| 分类号 |
F42B4/08;(IPC1-7):F42B4/08 |
主分类号 |
F42B4/08 |
| 代理机构 |
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代理人 |
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