DEVICE FOR PRESSURIZING PROPELLANT TANKS OF A ROCKET ENGINE
    1.
    发明申请
    DEVICE FOR PRESSURIZING PROPELLANT TANKS OF A ROCKET ENGINE 审中-公开
    用于压缩发动机的推进剂罐的装置

    公开(公告)号:US20160177874A1

    公开(公告)日:2016-06-23

    申请号:US14909894

    申请日:2014-07-25

    Applicant: SNECMA

    Abstract: The device comprises two heat exchangers (74, 90) suitable respectively for vaporizing first and second propellants before they are reintroduced in gaseous form into their tanks (16, 18). The heat exchangers co-operate respectively with first and second gas generators (60, 84) suitable for being fed with a mixture of propellants in order to produce combustion, the second gas generator (84) being suitable for being fed at least in part by the exhaust from the first gas generator (60).

    Abstract translation: 该装置包括两个热交换器(74,90),它们分别适于在将第一和第二推进剂以气态重新引入其储罐(16,18)之前蒸发。 所述热交换器分别与适于供给燃料混合物的第一和第二气体发生器(60,84)配合以产生燃烧,所述第二气体发生器(84)适于至少部分地由 来自第一气体发生器(60)的排气。

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