发明名称 |
METHOD OF WITHDRAWING ACCELERATING ROCKET MODULE FROM SPACESHIP FLIGHT PATH |
摘要 |
FIELD: transport.SUBSTANCE: invention relates to aerospace engineering, particularly, to rocket acceleration module and its components intended for its stabilisation and withdrawal from separated spaceship. Proposed method comprises issuing command for accelerating module engine shutdown and issuing command with time delay ?tfor separating accelerating module from spaceship and imparting them a relative velocity. It comprises also issuing the command for actuation of accelerating module withdrawal system to separate said module from spaceship with time delay ?t. Prior to issuing command for accelerating module engine shutdown at preset flight parameters of spaceship, the latter and accelerating module are oriented relative to preset transverse axis at position of separation and stabilised at said position. Withdrawal of accelerating module is combined with spinning it relative to common longitudinal axis.EFFECT: decreased weight of separation hardware.1 dwg |
申请公布号 |
RU2478064(C2) |
申请公布日期 |
2013.03.27 |
申请号 |
RU20110114479 |
申请日期 |
2011.04.13 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "RAKETNO-KOSMICHESKAJA KORPORATSIJA "EHNERGIJA" IMENI S.P. KOROLEVA" |
发明人 |
KOKUSHKIN VJACHESLAV VJACHESLAVOVICH;BORZYKH SERGEJ VASIL'EVICH |
分类号 |
B64G1/26 |
主分类号 |
B64G1/26 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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