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。
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.
出处
《固体火箭技术》
EI
CAS
CSCD
1992年第3期65-70,共6页
Journal of Solid Rocket Technology
关键词
火箭发动机
旋转试验
数据采集
Solid rocket engine
Rotating test
Surveying equipment
Computer control system
Data acquisition system
