首先印度完全是自力更生,从超级计算机到低温火箭发动机到地球静止轨道运转工具。
Firstly, the Indian effort is vastly home-grown, right from supercomputers to cryogenic engines to geosynchronous launch vehicles.
在低温液体火箭发动机的试验中,对液体密度的测量是很重要的。
It is very important to measure liquid density in cryogenic liquid rocket engine test.
研究了低温推进剂液体火箭发动机供应管道系统充填过程的建模问题。
The priming process of feed lines of cryogenic propellant liquid rocket engines was studied.
介绍了基于故障树分析法(FTA)进行的某固体火箭发动机低温下点火延迟故障的分析过程。
The ignition delay fault of solid rocket motor happening in a low temperature based on FTA is analyzed in the paper.
通过压力、高低温循环等大量的试验和理论分析表明:采用填充密封胶的螺纹联接密封结构具有优异的密封性,适宜在固体火箭发动机环境中应用。
Based on pressure and high low temperature cycling tests and theoretic analysis, the threaded joint parts filled with sealing glue compound show excellent seal ability, and can be applied to SRM.
应用领域涉及宇航,燃气涡轮,火箭发动机,太空船,航天飞机,核反应堆,涡轮泵密封件和低温贮藏容器。
Aerospace, gas turbines, rocket motors, spacecraft, space shuttles, nuclear reactors, turbo pump seals and cryogenic storage tank.
应用领域涉及宇航,燃气涡轮,火箭发动机,太空船,航天飞机,核反应堆,涡轮泵密封件和低温贮藏容器。
Aerospace, gas turbines, rocket motors, spacecraft, space shuttles, nuclear reactors, turbo pump seals and cryogenic storage tank.
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