发明名称 INSPECTION MONITORING DEVICE FOR ROCKET IN LAUNCHING RANGE
摘要 PROBLEM TO BE SOLVED: To improve workability of inspection work and reduce a work period by transmitting information related to each inspection portion of a rocket by radio transmission to a monitoring facility provided on the ground. SOLUTION: Various sensors and many avionics apparatuses 3 which are installed in a rocket is connected with a computer 11 for inspection and monitoring via data transmission cables 4, a radio communicating transceiver 12 is connected with the computer 11, and a transceiver 21 and a large-sized computer 22 are installed in a launch control car. Automatic sequence control for monitoring that each maintenance work is progressed as expected in parallel with an operation work and automatic checkout for each avionics apparatus 3 are performed. The automatic sequence control function is judged abnormal when a certain work does not finish within an expected period, the automatic checkout function is judged abnormal when any avionics apparatus 3 measures a figures exceeding a tolerance, and the contents are transmitted to the large- sized computer 22 on the ground.
申请公布号 JP2000085700(A) 申请公布日期 2000.03.28
申请号 JP19980262100 申请日期 1998.09.16
申请人 ISHIKAWAJIMA HARIMA HEAVY IND CO LTD 发明人 MIZUKOSHI NORIYOSHI
分类号 B64G5/00;(IPC1-7):B64G5/00 主分类号 B64G5/00
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