rocket-ramjet engine 中文意思是什麼
rocket-ramjet engine
解釋
火箭沖壓式發動機-
As the air - breathing engine, the performance of solid rocket ramjet is determined not only by structure of engine and the performance of propellant, but also by flight condition
作為吸氣式發動機,其性能不僅取決于發動機本身結構和推進劑性能,與飛行狀態也有密切的聯系。 -
According to the definition and expression of the thrust, as well as the condition derived from them, a method of solid rocket ramjet thrust determination and its program are provided on the basis of engine ground simulation test
本文以西北工業大學固體火箭沖壓發動機直連式試車臺為研究對象,探討固體火箭沖壓發動機地面試驗技術。首先,從推力的定義出發,建立了試驗中來流空氣流量、燃料流量與固體火箭沖壓發動機推力之關系。 -
The determination of solid rocket ramjet thrust and testing method are the important basis of the developing engine. an experimental program evaluating solid rocket - ramjet in nwpu connected - pipe facility is underway
我國發展中遠程、超音速導彈計劃已經啟動,其動力裝置首選固體火箭沖壓發動機,而地面試驗技術是發動機研究重要基礎。 -
All of the work made foundation of developing solid rocket - ramjet engine
為固體火箭沖壓發動機試驗研究打下基礎。 -
The research project of the middle - long and hypersonic missile with solid rocket - ramjet engine has been launched. the measurement and control technologies are the important basis of developing engine, which is one of the key technologies of the research
我國發展中遠程、高超聲速固體沖壓導彈已經啟動,其關鍵技術之一是研製性能優良的固體火箭沖壓發動機,而試驗測控技術是發動機研製中不可或缺的重要基礎。 -
Integral rocket - ramjet is a propulsion system with great potential. using missile - engine integrated design method to realize the conceptual design of integral rocket - ramjet missile is of great significance to improve quality and efficiency of missile design
整體式火箭沖壓發動機是一種很有前途的動力裝置,採用導彈和發動機一體化設計方法進行整體沖壓式導彈的總體設計,對于提高導彈的設計質量和設計效率具有重要的意義。
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