... 固体推进剂火箭 solid-propellant rockets 固体推进剂马达 solid-propellant motors 高能固体推进剂 high energy solid propellant ...
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... 固体推进剂马达 solid-propellant rockets 固体推进剂火箭 solid-state measurements 固态聚合 solidification ...
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固体推进剂火箭发动机 solid propellant engine
中国从1958年开始复合固体推进剂火箭发动机的探索和研制工作。
China has undertaken to research and develop composite solid propellant rocket motors since 1958.
人们已经用过各种类型的机械控制面来偏转固体推进剂火箭的排气流。
A variety of mechanical surfaces have been employed for deflecting the exhaust jets of solid-propellant rockets.
推进剂的羽焰温度是固体推进剂火箭发动机的重要参数，对于研究发动机内的燃烧过程具有重要价值。
The plume temperature is an important parameter, for solid propellant rocket engines and it is useful for determining the combustion process of the engine.
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