Propellant property and nozzle closure opening pressure have an important effect on the ignition transient.
推进剂的燃烧特性及喷管堵盖打开压强对点火升压过程有较大影响。
The results also show that the structure of chelated titanate has large effect on processability of the propellant.
结果还表明螯合型钛酸酯的结构变化对推进剂工艺性能影响较大。
Conclusion Chronic effect, induced by liquid rocket propellant, was observed in our study.
结论液体火箭推进剂致伤后的远期效应明显。
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