A new calculation method was proposed for the typical structure of the platelet transpiration flux in the rocketthrust 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。
2
A piezoelectricity measuring system used for measuring rocketthrust vector is introduced. A devices to static accomplish, calibration and dynamic calibration on the system is designed.