摘要
分析了空间飞行器推进剂贮箱并联设置时产生的不平衡输出问题,从工程角度估计了不平衡输出的程度。对于不允许测量贮箱压降的金属膜片贮箱。
This paper analyzes the unbalanced output of flow at the exit of parallel arranged tanks of space vehicle, and estimates the degree of unbalanced output from the aspect of engineering. As the measurement of pressure drop of metal diaphragm tank is not allowed, installation of the cavitating veturi at the exit of tank is a simple and effective method to solve the unbalanced output of flow.
出处
《上海航天》
2000年第1期8-11,共4页
Aerospace Shanghai
关键词
气蚀管
飞行器
推进剂贮箱
不平衡输出
Propellant tank
Propulsion system
Cavitating venturi
Space vehicle
