Parameters and Trajectory Overall Optimization Design of the Combined Cycle Engine Reusable Launch Vehicle

作     者：CUI Naigang ZHAO Lina HUANG Rong WEI Changzhu 

作者机构：School of Astronautics of Harbin Institute of Technology Harbin 150001 China Academy of Launch Vehicle Technology Beijing 100076 

出 版 物：《中国航天：英文版》 (Aerospace China)

年 卷 期：2016年第17卷第4期

页      码：14-20页

摘      要：Reusable launch vehicle is an important way to realize fast,cheap and reliable space transportation.A combined cycle engine system provides a more efficient and flexible form of *** investigation on the research status of the combined cycle engine technology,including basic principle,research programs and classification of structure is firstly discussed in this *** the bilevel hierarchical and integrated parameters/trajectory overall optimization technologies are applied to improve the efficiency and effectiveness of overall vehicle *** are implemented to compare and analyze the effectiveness and adaptability of the two algorithms,in order to provide the technical reserves and beneficial references for further research on combined cycle engine reusable launch vehicles.

主 题 词：可重复使用运载器 发动机系统 联合循环 整体优化设计 发动机技术 空间运输 动力形式 结构分类 

学科分类：080703[080703] 08[工学] 082502[082502] 0807[工学-电子信息类] 0825[工学-环境科学与工程类] 

馆 藏 号：203225803...