In this paper, the Micro chemical Thruster's structure was designed and loading method of propellant and test method of thrust were investigated.
该文设计了化学微推力器的结构,研究了微推力器的装药方法和推力的测试方法。
A new calculation method was proposed for the typical structure of the platelet transpiration flux in the rocket thrust chamber based on the test data of another chamber.
针对典型的层板发汗冷却结构,提出了利用一个推力室的实验数据来计算另一推力室所需发汗流强的方法。
In this paper, a simple method for analysis of ground test data of the solid rocket motor with reversal nozzles is presented based on solving the reverse thrust at an altitude from ground test data.
文中介绍了根据地面实验数据分析反喷管在高空提供的反推力,为带反喷管发动机地面实验数据处理提供了简便的分析方法。
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