... 高温风洞 high-temperature tunnel 高温推进剂 high-temperature propellant 高性能飞机 high performance airplane ...
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The temperature of a high temperature, high pressure plume solid propellant rocket engine is difficult to measure but is useful for determining the combustion status of the engine.
对于固体火箭发动机羽焰温度的测量是困难的，了解其温度分布对于研究发动机内燃烧流场的特性有重要价值。
It is shown that compounds of borate especially borate 5527 is available to improve the mechanical performance of HTPB propellant at high temperature.
尤其是硼酸酯化合物5527，能大幅度提高高温力学性能，是优异的丁羟推进剂新型偶联剂。
The low temperature sensitivity coefficient (LTSC) effect of high energy nitroamine propellant through the closed vessel and interior ballistic experiments is studied.
通过中止试验、高压密闭爆发器试验与火炮内弹道试验研究了低温感高能硝胺发射药的低温感效果。
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