The chamber successfully achieved a full thrust of 100000 Ibf.
腔室成功达到了100000 Ibf 的全推力。
2
Then using this method, influence of gas wall material, gas wall thickness and flow rate of coolant on regenerative cooling of thrustchamber was investigated. The results were satisfactory.
然后使用这种方法研究了气壁材料、气壁厚度和冷却液流量对推力室再生冷却的影响,获得了比较满意的结果。
3
And then, as now, the heart of the system will remain the thrustchamber.