| 发明名称 |
SPACECRAFT DOCKING DEVICE |
| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to space engineering. Spacecraft docking device comprise active unit with docking mechanism arranged at its center and passive unit with mate intake cone terminated in mount. Said intake cone is composed by nozzle of sustainer rocket engine of separable last stage of spaceship. Docking mechanism is composed of telescoping bars with free end furnished with spring-loaded parasol-shaped lugs arranged to unlock and lock.EFFECT: simplified docking.4 dwg |
| 申请公布号 |
RU2490183(C1) |
申请公布日期 |
2013.08.20 |
| 申请号 |
RU20120108867 |
申请日期 |
2012.03.07 |
| 申请人 |
FEDERAL'NOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "OMSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET" |
发明人 |
TRUSHLJAKOV VALERIJ IVANOVICH;JUTKIN EVGENIJ ALEKSEEVICH;TJUTEBAEV TALGAT KENZHEBAEVICH;SHATROV JAKOV TIMOFEEVICH;MAKAROV JURIJ NIKOLAEVICH |
| 分类号 |
B64G1/64;F42B15/36 |
主分类号 |
B64G1/64 |
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