ROCKET LAUNCHER
    1.
    发明专利

    公开(公告)号:JPH0192560A

    公开(公告)日:1989-04-11

    申请号:JP24961787

    申请日:1987-10-02

    Abstract: PURPOSE:To improve combustion efficiency in a rocket having two kinds of fuel and liquid for propulsion agent by providing a fuel jet for sending atomized main liquid fuel info sub-fuel jet jetted under the gasified state and a liquid oxygen jet coaxial with said fuel jet. CONSTITUTION:In a rocket engine liquid oxygen, kerosene and hydrogen respectively for oxidizing agent, fuel and sub-fuel, liquid hydrogen 4 as sub-fuel is sent by a pump 8, and a portion of the sub-fuel is jetted from an injector 1 into a combustor 5, while the remaining is sent to a high temperature gas generator 6 to be burnt with the liquid oxygen 2 being supplied by a pump 8'. Pumps 8-8'' are driven through turbines 7, 7' with high temperature gas generated by said generator 6. Main fuel 3 is forced into the combustor 5 by the pump 8''. Then, the main fuel 3 and liquid oxygen 2 are jetted into the combustor 5 respectively from a jet 13 and an oxygen jet 12 provided in the center of a jet 14. A hydrogen jet 14' is opened to the upstream side wall of jet 14 to supply the sub-fuel 4.

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