High performance liquid rocket propellant
    96.
    发明授权
    High performance liquid rocket propellant 有权
    高性能液体火箭推进剂

    公开(公告)号:US09359974B2

    公开(公告)日:2016-06-07

    申请号:US14224214

    申请日:2014-03-25

    Inventor: Indresh Mathur

    Abstract: Disclosed is a process of fueling a rocket engine or air-breathing engine for a hypersonic vehicle with a high performance hydrocarbon fuel characterized by a hydrogen content greater than 14.3% by weight, a hydrogen to carbon atomic ratio greater than 2.0 and/or a heat of combustion greater than 18.7 KBtu/lb. The disclosed fuels generally have a paraffin content that is at least 90% by mass and a C12-C20 isoparaffin content of at least 40% by mass.

    Abstract translation: 公开了一种用于具有高于14.3重量%的氢含量大于2.0的氢含量和/或热量的高性能烃燃料的高性能车辆的火箭发动机或空气呼吸发动机的过程, 的燃烧量大于18.7 KBtu / lb。 所公开的燃料通常具有至少90质量%的链烷烃含量和至少40质量%的C 12 -C 20异链烷烃含量。

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