Ascend motion analysis of reusable launch vehicle 可重復(fù)使用運載器上升段運動分析
Technical progress of reusable launch vehicle part 國外可重復(fù)使用運載器的技術(shù)進展
A study of the two - stage - to - orbit reusable launch vehicle scheme 兩級入軌重復(fù)使用運載器的方案探討
Ceramic thermal protection system for reusable launch vehicle 地鐵供電系統(tǒng)設(shè)備選擇與全壽命周期費用的關(guān)系
Design of variable - structure attitude control system for rlv reusable launch vehicle 可重復(fù)使用運載器變結(jié)構(gòu)姿態(tài)控制算法設(shè)計
Review past nasa and air force attempts to develop a reusable launch vehicle 回顧過去美國太空總署和美國空軍嘗試發(fā)展可回收發(fā)射載具。
The predictor - corrector reentry guidance algorithm for reusable launch vehicles was studied 摘要研究了可重復(fù)使用運載器的預(yù)測校正再入制導(dǎo)方案。
The group project will be a study of the technological , architectural , and policy options associated with developing a new reusable launch vehicle 這個團體專題是發(fā)展一種新型可回收的發(fā)射載具以所面臨相關(guān)的技術(shù)與架構(gòu),以及政策方案。
In this paper , flight trajectories were designed for a small - scale model of a reusable launch vehicle ( rlv ) according to the dropping missions 摘要根據(jù)投放任務(wù)要求設(shè)計縮比可重復(fù)使用空間飛行器( rlv )投放軌跡,并建立飛行動力學(xué)基本分析框架。