CAJ | 학술논문

为了研究弹用涡轮喷气发动机动态启动加速过程，开展了发动机火箭橇试验研究。通过火箭橇试验，可掌握导弹发射条件下弹用涡轮喷气发动机启动加速特征，暴露发动机在启动加速方面的设计缺陷。火箭橇试验能够真实的模拟导弹发射条件，它对于弹用涡轮喷气发动机研究具有十分重要的意义。
위료연구탄용와륜분기발동궤동태계동가속과정，개전료발동궤화전취시험연구。통과화전취시험，가장악도탄발사조건하탄용와륜분기발동궤계동가속특정，폭로발동궤재계동가속방면적설계결함。화전취시험능구진실적모의도탄발사조건，타대우탄용와륜분기발동궤연구구유십분중요적의의。
The rocket sled test was carried out for overall investigatingthe dynamic process of missile turbojet engine starting and accelerating. The character istics of the dynamic process of starting and accelerating were mastered by the rocket sled test and some design mistakes were exposed also. The rocket sled test can imitate the dynamic conditions of missile launching, it is very important for missile turbojet engine design.