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。
2
The typical measurement data are given and a comparision is made with type BZD-2 parallel electrode neutron chamber.
给出了典型的测试数据，并与BZD-2型平板形电极电离室进行了对比。
3
The objective of these studies is to gather data that enable them to adapt the test chamber for ramjet tests.