摘要
介绍了一种适用于飞行器在负过载情况下启动的新型增压输送系统,该系统采用气液隔离方式,比国外可重复使用飞行器的增压输送系统结构质量轻、体积小,有利于提高飞行器的性能。分析了该系统的特点,给出了系统的主要性能参数。新型增压输送系统经过冷流试验和热试车的考核,结果均满足设计和使用要求。
This paper presents a new pressurization and propellant feed system for aircraft start-up under negative G condition. The system is of light structural weight and small volume and uses a kind of gas-liquid isolation system. The characteristics of this system were analyzed, and some main performance parameters were given. Cold-flow test and hot test were performed to test the performance of this system, test results show that this new system can satisfy designed objective and meet the practical requirements.
出处
《火箭推进》
CAS
2007年第2期12-16,共5页
Journal of Rocket Propulsion
关键词
负过载
隔膜
增压输送
negative G
metallic septum
pressurization and propellant feed