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A fast engineering algorithm of Microwave Plasma Thruster (MPT) performance prediction was presented.
对微波等离子推进器提出一种快速性能预估的工程算法。
The results can provide reference for the testing of MPT vacuum plume and integral design of spacecraft.
计算结果对以后MPT真空羽流场测试和航天器一体化设计提供了参考。
The MPT Series features close-coupled construction similar to the MP Series, but uses a regenerative turbine vane impeller.
该设备结构紧密,除了使用一款回热式透平推进器以外,与MP系列泵很相似。
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