... 发热量 heat productivity; calorific ... 固体推进剂发动机 solid-propellant engine 混合推进剂发动机 hybrid-propellant engine ...
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solid propellant engine 固体推进剂火箭发动机
solid-propellant rocket engine 固体火箭发动机
solid-propellant boost engine 固体推进剂助推发动机
solid propellant socket engine 固体推进剂火箭发动机
solid propellant locket engine 固体推进剂火箭发动机
solid-propellant t rocket engine 固体火箭发动机
The propellant feature of burning behavior and engine in hybrid engine, the differences to liquid and solid engine and the difficulties of technology in development were analyzed.
分析了固液发动机推进剂的燃烧特性和发动机性能特性、与液体和固体火箭发动机的不同，以及研制的技术难度等。
To find out the performance characteristic of aerospike nozzle, the simulated tests were a aerospike engine unit using solid propellant.
为了了解塞式喷管性能，采用固体推进剂对塞式喷管单元发动机进行了模拟实验。
The plume temperature is an important parameter, for solid propellant rocket engines and it is useful for determining the combustion process of the engine.
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。
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