单室双推力火箭发动机
Based on the investigation of thrust measurement technique for a rocket engine, a improved method for solving the thrust measurement in the test of the solid rocket engine with single-chamber and. dual-thrust was presented in the paper.
本文通过对某单室双推力发动机推力测试技术的探讨,提出了解决单室双推力固体火箭发动机推力测试技术的改进方法。
Using the single chamber dual thrust rocket engine explosion of gas flow temperature field simulation environment, the storage unit to verify the test experiments, the test unit can store a complete record of temperature data.
最后,利用单室双推力火箭发动机燃气流场模拟爆炸温度场环境,对存储测试单元性能进行了验证实验。实验结果表明,存储测试单元能够完整的记录温度变化的数据。
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