摘要
分析了1Cr18Ni9Ti与MON- 3 液体推进剂相容性的机理,对用1Cr18Ni9Ti软管加注MON- 3 液体推进剂的可行性进行了探讨。
The mechanism of compatibility of 1Cr18Ni9Ti with liquid propellant MON-3 is analysed. A probe on practicability of using 1Cr18Ni9Ti hose for loading liquid propellant MON-3 is conducted.
出处
《导弹与航天运载技术》
1999年第5期29-31,共3页
Missiles and Space Vehicles
关键词
液体火箭
推进剂
相容性
四氧化二氮
Liquid propellant, + MON-3 propellant, Propellant compatibility.