新一代运载火箭助推器分离验证试验技术  

Test technology for rocket booster separation of new generation launch vehicle

作　　者：张建华[1] 皮本楼[1] 王佳南[1] 崔高伟[1] 刘陆广[1] ZHANG Jianhua;PI Benlou;WANG Jianan;CUI Gaowei;LIU Luguang(Beijing Institute of Structure and Environment Engineering, Beijing 100076,China)

机构地区：[1]北京强度环境研究所,北京100076

出　　处：《强度与环境》2017年第4期1-9,共9页Structure & Environment Engineering

摘　　要：助推器分离验证试验是新一代运载火箭研制过程中非常重要的大型地面试验之一。本文介绍了助推器分离试验的目的、总体设计思路、试验方案、关键技术和实验效果,该项技术运用在新一代运载火箭研制过程中,两种新研发的回收技术和分离试验综合仿真技术的成功应用使大型助推器分离方案验证试验取得了圆满成功,为将来重型运载火箭助推器分离试验技术提供技术支撑。Rocket booster separation test is very important during the development of new generation launch vehicle.A new test technology was studied,and it was applied to rocket booster separation experiment of new generation launch vehicle,and indicated the improvement of heavy launch vehicle booster separation ground testing technology.

关 键 词：助推器 分离试验 回收气囊 刹车缓冲 

分 类 号：V43[航空宇航科学与技术—航空宇航推进理论与工程]