摘要
对用于低温液氧推进剂的表面张力贮箱进行了理论上的初步分析,认为其在理论上是可以实现的。从低温表面张力贮箱的材料选择、低温推进剂引起的热应力及隔热层结构形式等方面进行了初步探讨。重点介绍了低温表面张力贮箱隔热层的结构形式及选用的隔热材料。分析了低温表面张力贮箱面临的特殊问题。
The cryogenic surface tension LOX tank is theoretically analyzed. The key design parameters such as tank material selection, cryogenic propellant caused structure thermo stress and heat insulation structure are discussed. Insulation layer types and their materials of the tank are introduced. Some special problems are also analyzed.
出处
《火箭推进》
CAS
2005年第3期26-29,共4页
Journal of Rocket Propulsion
关键词
表面张力贮箱
低温推进剂
隔热
surface tension propellant tank
cryogenic propellant
heat insulation
