1) ejector rocket motor
引射火箭发动机
1.
Based on comprehensive analysis for combustion mode of ejector rocket,the numerical analysis of SMC+DAB hybrid combustion mode and direct connected experiments for the ejector rocket motor with fixed structure were carryied out by means of the essential principle of dual-combustor ramjet.
在综合分析引射火箭燃烧组织模式的基础上,针对固定结构的引射火箭发动机,借助双燃烧室冲压发动机的原理,开展了SMC+DAB混合燃烧组织模式的数值分析和发动机直连实验研究,详细分析了富燃一次燃气对二次燃烧火焰稳定的作用及其对发动机性能的影响。
2) rocket igniter
火箭发动机引火器
3) Rocket-based combined cycle (RBCC)
支板火箭引射冲压组合发动机
4) lighting,chemical fuel motor,rocket,rocket engine,rocket motor,thrust chamber,rocket engine,rocket-motor compartment,thrust cylinder,rocket powerplant,rocket propulsion
火箭发动机，发射<火>
5) jet wash
喷气火箭发动机射流<火>
6) Rocket engine
火箭发动机
1.
Design of diagnostic knowledge mining system for liquid propellant rocket engine;
液体火箭发动机诊断知识挖掘系统设计
2.
Modeling and analysis for dynamic thrust testing system of orbit/attitude control rocket engine;
轨/姿控火箭发动机推力动态测试系统建模分析
3.
Investigation of GO_2/kerosene thrust chamber of the main rocket engine for the RBCC propulsion system
RBCC推进系统主火箭发动机气氧/煤油推力室研究
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条