| 发明名称 |
SPACE HEAD FOR GROUP LAUNCH OF SATELLITES |
| 摘要 |
FIELD: transport. ^ SUBSTANCE: invention relates to rocketry. Space head for group launch of satellites comprises adapter module for docking to rocket last stage, satellite attachment module and nose cone. Individual launch units are added made up of platform, instrument module and engine, to be docked to each satellite by means of pyro bolts. ^ EFFECT: possibility to launch both low- and high-orbit satellites by one rocket. ^ 2 dwg |
| 申请公布号 |
RU2428358(C1) |
申请公布日期 |
2011.09.10 |
| 申请号 |
RU20100101957 |
申请日期 |
2010.01.22 |
| 申请人 |
FEDERAL'NOE GOSUDARSTVENNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA VOENNAJA AKADEMIJA RAKETNYKH VOJSK STRATEGICHESKOGO NAZNACHENIJA IMENI PETRA VELIKOGO MO RF |
发明人 |
GIMADIEV RAFAEHL' RAFIKOVICH;EVSEEV IGOR' VALENTINOVICH;KOPYLOV OLEG ANDREEVICH |
| 分类号 |
B64G1/22 |
主分类号 |
B64G1/22 |
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