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小型固体发动机旋转试验用微型点火控制与数据采集系统
引用本文:汪亮,李波.小型固体发动机旋转试验用微型点火控制与数据采集系统[J].固体火箭技术,1992(3).
作者姓名:汪亮  李波
作者单位:西北工业大学,中国人民解放军二炮四所 西安 710072,北京 100000
摘    要:为适应固体火箭发动机旋转试验的需要,以MCS—96单片机为主机,设计了一种微型的点火控制与数据采集系统。该系统直接安装在旋转试验台内部。省去了传统的集流环,为以后开展悬浮试验创造了条件。

关 键 词:固体火箭发动机  旋转试验  测试设备  计算机系统控制  数据采集系统

MINIATURE SYSTEM OF IGNITION CONTROL AND DATA COLLECTION FOR ROTATAING TEST OF SMALL SRM
Wang Liang,Li Bo Northwestern Polytechnical University,Xian, th Research Institute of the Second Artillery,the PLA of China,Beijing.MINIATURE SYSTEM OF IGNITION CONTROL AND DATA COLLECTION FOR ROTATAING TEST OF SMALL SRM[J].Journal of Solid Rocket Technology,1992(3).
Authors:Wang Liang  Li Bo Northwestern Polytechnical University  Xian  th Research Institute of the Second Artillery  the PLA of China  Beijing
Institution:Wang Liang,Li Bo Northwestern Polytechnical University,Xian,710072 4th Research Institute of the Second Artillery,the PLA of China,Beijing,100000
Abstract:To meet the needs of rotating tests of the solid rocket motor array, a min- iature system of ignition control and data collection is designed based on the dingle chip microcontroller MCS-96. The system is directly installed within the rotating test fixture. Dispensing with the traditional collector ring, the system creates favourable condition for the future levitation test.
Keywords:Solid rocket engine  Rotating test  Surveying equipment  Computer control system  Data acquisition system
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