... 申请人: Societe Europeenne de Propulsion 代理人: Weingarten, Schurgin, Gagnebin & Hayes LLp 发明名称: Pulse rocket engine ...
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pulse detonation rocket engine 脉冲爆震火箭发动机
Solid rocket pulse engine 固体火箭脉冲发动机
pulse solid rocket engine 脉冲固体火箭发动机
Firstly, the pulse rocket engine test system has been built and provides hardware constitute plan and test every aspect of the application of the test.
本文首先对脉冲火箭发动机的测试系统进行组建，提出了测试系统的硬件组成方案，并对测试系统的各个应用环节加以论证。
A prototype of pulse detonation rocket engine (PDRE) is introduced to solenoid valves for the control of oxygen, kerosene and isolation gas; thus continuous combustion is avoided.
简述了脉冲爆震火箭发动机的实验系统，利用电磁阀控制煤油，氧气和隔离气体，避免了连续燃烧。
A pulse detonation rocket engine (PDRE) is a new propulsion system that generates thrust by using high-temperature and high-pressure air produced by pulse detonation waves.
脉冲爆震火箭发动机是一种利用脉冲式爆震波产生高温、高压燃气发出的冲量来产生推力的新型推进系统。
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