Results of subscale engine test show that the insulation (PFDH-2) can be used for heat protection of oxidizer rich solid rocket enginechamber.
试车结果表明，PFDH - 2绝热层可以对富氧环境下工作的发动机燃烧室实施有效热防护。
2
The simulation result indicates that the simulation of the enginechamber performances by using Monte-Carlo method is feasible and that the non linear model is accurate enough.
仿真结果表明，利用M - c方法对推力室进行数值仿真是完全可行的，所用的非线性模型是足够准确的。
3
A calculation of the wall temperature distribution in liquid propellant rocket enginechamber with milled grooves was completed by the aid of three-dimensional finite element method.