实验数据是由一个计算机化六分力式数据采集系统采集的。
The data were collected by a computer based stationary six-cell dynamometer data acquisition system to measure the forces on the rod.
采用六分力试验技术对某推力矢量发动机燃气舵的气动特性进行了试验研究。
Computational investigation of secondary flow thrust vector control technology used in a convergent-divergent nozzle;
本文用最大误差方法，对固体火箭发动机六分力立式试验台的静态误差进行了分析。
By using the method of maximum error, the paper deals with the analysis of the static error of the six-component force test stand of solid rocket motors.
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