rocket-ramjet

基本解釋

All of the work made foundation of developing solid rocket-ramjet engine.
為固體火箭沖壓發(fā)動機試驗研究打下基礎。
The theoretical specific impulse formula for two-phase flow in nozzle of rocket-ramjet engine is derived on the basis of similarity to that used for rocket engine.
本文導出了類似于火箭發(fā)動機的火箭沖壓發(fā)動機噴管的兩相流動理論比沖公式；
hkxb.buaa.edu.cn
The research of the high-powered solid rocket-ramjet engine has been launched, which is one of the key technologies of the middle-long and supersonic missile project.
我國發(fā)展中遠程、超音速導彈計劃已經(jīng)啟動，其動力裝置首選固體火箭沖壓發(fā)動機，而地面試驗技術是發(fā)動機研究重要基礎。