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高比冲
    Research on the High Specific Impulse Bipropellant Liquid Apogee Engine
    高比冲双组元液体远地点火箭发动机研究
    The scramjet has some advantages of high flow velocity, high specific impulse and wide operating range which become a viewpoint in the research field of power of Aeronautics and Astronautics.
    超燃冲压发动机以其高速、高比冲和工作范围宽广的特点,正逐渐成为当今航空航天动力领域的研究焦点。
    Stationary plasma thruster (SPT) is a kind of advanced electric propulsion concept. Because of its high specific impulse, high efficiency, small bulk and low weight, it is being widely used in tasks such as pose control, orbit correct, position retain, and so on.
    稳态等离子发动机(SPT)是一种先进的电推进技术,具有高比冲、高效率、体积小、重量轻等特点,广泛应用于航天器姿态控制、轨道修正、位置保持等任务。
    According to theoretical and experimental results achieved up to date, it is concluded that MPT is a kind of advanced thruster with high specific impulse, long lifetime, low thrust and thus especially fitting for space propulsion such as orbit transfer, attitude control, station keeping, docking and rendezvous, planetary.
    分析现有理论与实验研究结果后认为,MPT是一种高比冲、长寿命的小推力动力装置,特别适合用作空间动力,进行航天器的轨道转移、姿态控制、位置保持、对接交会和星际航行。
    Arcjet is the highlight of investigation and application in world because of its high specific impulse, high ratio of thrust and power.
    电弧等离子体发动机 (Arcjet)因其高比冲、高推力 功率比等特点成为当前国际上电火箭研究和应用的热点。
    This paper discusses the advantage using high specific impulse electric rocket as primary propulsion of spacecraft.
    本文讨论了除改善现用化学推进系统性能外,采用高比冲电火箭发动机担负探测器主推进的优越性。
 

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