Total impulse is one of the most important parameters which is highly related to the
performance of solid rocket motors. Predicting the total impulse accurately is necessary for …

This paper aims to introduce a new technique to eliminate the erosive burning phenomenon
in solid rocket motors. The erosive burning which occurs in motors with high volumetric …

Solid rocket motors (SRMs) have been a critical component of space exploration, military
operations, and numerous other applications for decades. The ability to accurately predict …

基于火箭撬地面试验的需要, 设计了大载荷高加速的短轨火箭橇动力系统, 并对地面效应对火箭
发动机尾喷管流场的影响进行了理论和试验研究. 文中采用FLUENT 计算软件对不同条件下的 …

Despite the short duration, ignition transient plays a very important role in the whole
operation of a solid rocket motor. A two-dimensional model is proposed to simulate the …

This paper describes a zero‐dimensional model for evaluating the mass flow rate history of
a solid rocket motor igniter. Based on the results of an igniter‐firing experiment, in which the …