1) Solid Rocket Ramjet
固冲发动机
1.
During the study of Solid Rocket Ramjet (SRR), ablation of afterburner thermal insulation is a serious problem, which cannot be ignored.
固冲发动机补燃室绝热层的烧蚀问题是目前固冲发动机研制过程中所面临的一个重要问题。
2) solid ramjet
固冲发动机
1.
The necessity of flow regulation system in solid ramjet is presented,and the scheme of gas-fired flux adjustment about generator is analyzed.
阐述了固冲发动机燃气流量调节的必要性,对发生器燃气流量调节方案进行了评述。
3) solid rocket engine specific impulse
固体发动机比冲
4) solid propellant ramjet
固体冲压发动机
1.
Study on the C/SiC composites for hot gas valve of solid propellant ramjet;
固体冲压发动机燃气阀用C/SiC复合材料研究
5) solid rocket ramjet
固体火箭冲压发动机
1.
Quick-forecasting algorithm for performance of solid rocket ramjet;
固体火箭冲压发动机性能快速预估算法
2.
Some technological problems of solid rocket ramjet;
固体火箭冲压发动机的若干技术问题
3.
Experimental study on solid rocket ramjet with central air-inlet mode;
中心进气式固体火箭冲压发动机试验研究
6) solid fuel ramjet
固体燃料冲压发动机
1.
Analysis on thrust stationarity and flight stability of solid fuel ramjet;
固体燃料冲压发动机推力平稳性及飞行稳定性分析
2.
Influence of vortex on performance of solid fuel ramjet;
涡流对固体燃料冲压发动机性能影响分析
3.
Structure design on torch igniter of solid fuel ramjet;
固体燃料冲压发动机火炬式点火器设计
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