航天飞行器微重力试验技术综述  

Review of Micro-Gravity Test Technology for Aerospace Vehicle

作　　者：贾洲侠[1] 王梦魁[1] 李海波[1] 张伟[1] 王建军[1] 任方[1] JIA Zhou-xia;WANG Meng-kui;LI Hai-bo;ZHANG Wei;WANG Jian-jun;REN Fang(Science and Technology on Reliability and Environment Engineering Laboratory,Beijing Institute of Structure and Environment Engineering,Beijing 100076,China;Beijing Institute of Structure and Environment Engineering,Beijing 100076,China)

机构地区：[1]北京强度环境研究所可靠性与环境工程技术重点实验室

出　　处：《强度与环境》2019年第5期7-17,共11页Structure & Environment Engineering

基　　金：国家自然科学基金(11502023,11502024)

摘　　要：航天飞行器的液体管理问题是制约未来先进上面级、天地往返飞行器及轨道飞行器等先进飞行器推进剂利用效率以及可靠性的关键技术问题。本文针对近年来该领域的型号技术背景、主要技术问题以及相关的试验方法开展综述研究,重点分析了针对低温推进剂热管理的相关技术途径的研究进展。The propellant management problem for aerospace vehicle is one of the key reliability and efficiency issues for the development of advanced upper stage, reusable launch vehicle and orbiting craft. This paper aims in the progress of the engineering application background, main technical problems and test technology in the area of propellant management under micro-gravity condition. The emphasis is on the progress of thermal management issue for cryogenic propellants.

关 键 词：液体管理 低温推进剂 微重力 落塔 试验 

分 类 号：V421.33[航空宇航科学与技术—飞行器设计]