研究结果对该类推进剂配方设计和工艺参量选择提供了必要的实验依据。
The test results provide experimental basis for formula design and technological parameter selection of NEPE propellant.
这证明固体推进剂能量特性的优化设计是成功的，为固体推进剂配方设计提供了一种有效的计算方法。
The numerical results obtained agree fairly well with the results obtained by graphical method for determining the optimum composition of solid propel…
结果表明均匀设计在推进剂配方优化中的应用是可行的。
Results indicate it is practicable to apply even design method to select optimum formula for propellant.
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