头部载有记录火箭飞行路径和其他资料的摄录机和电子设备；尾部有温度和应变传感器。
The nosecone carried a video camera and avionics to record the rocket’s flight path and other information; the aft end, temperature and strain sensors.
然后，介绍了上位机软件设计以及上位机与温度记录仪之间的通信协议设计。
And then, the design of software in PC and communication protocol between PC and temperature logger are introduced.
当压缩机离合器合上时，记录排放空气温度和压缩机排放压力。
With the compressor clutch engaged, record the discharge air temperature and the compressor discharge pressure.
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