摘要
运用数学方法计算火箭发动机试验中推进剂在传输过程中的冷量损失,并与试验结果进行比较,验证了方法的有效性,为低温输送管路的设计提供依据。
Cool capacity loss in transportation of chemical propellant during the rocket engine test was calculated with math formulas. Compared with experiment result, the calculation method was proved effective and could be a solution for low temperature transport pipeline design.
出处
《低温工程》
CAS
CSCD
北大核心
2008年第2期59-61,共3页
Cryogenics
关键词
液氧
输送管路
冷量损失
liquid oxygen
transport system
cool capacity loss
