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Method and apparatus for testing of an operational marsch flight body in various prüfzenarien maintenance by means of operating mode
Method and apparatus for testing of an operational marsch flight body in various prüfzenarien maintenance by means of operating mode
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机译:通过运行模式在各种预维护中测试运行中的marsch飞行器体的方法和装置
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摘要
Device for the test of an operational missile consisting of• a umbilical - cable corresponding. Mil - std 1760,• a milbus - control unit (''bus control unit ′ corresponding. Mil - std 1553) with humans - machine - interface,• an rtu - addresses - bridges - circuit corresponding. Mil - std 1760,• an active gps - antenna including 12 v dc voltage - supply,• a gps - signal - extension for the missile - gps - antenna• a switchable 3 × 115 v 400 hz voltage - source,• a radar altimeter - signal - retardants,• an operation ellem cable to the maintenance device - flap of the missile to be tested• a bottle filled with coolant for the infrared - seeker head and a display screen,• a unit for missions - flat - charging,characterised by the following features:a. the umbilical cable - cable leads only the following signals: milbus - channel a, milbus - channel b, rtu - address - lines, 3 × 115 v 400 hz lines, gps - antennas - signal,example, the rtu - addresses - bridge circuit of the test device is bridged the rtu - address - lines of the umbilical - cable, so that there is for the missile to be tested an rtu - address that is, which mode used differently to the rtu - addresses..
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机译:用于测试运行中的导弹的设备,包括•脐带-电缆。 Mil-std 1760,•带有人机-机器-接口的milbus-控制单元(“总线控制单元'对应。mil-std 1553”),•rtu-地址-桥-电路对应。 Mil-std 1760,•有源gps-包括12 v dc电压的天线-电源,•a gps-信号-导弹扩展-gps-天线•3×115 v 400 hz可切换电压-源,•雷达高度计-信号-阻滞剂,•通往维护设备的操作杆电缆-被测导弹的襟翼•装有用于红外线的冷却剂的瓶子-搜寻头和显示屏,•用于任务的单元-扁平-充电,已特性化通过以下功能:a。脐带电缆-电缆仅引导以下信号:milbus-通道a,milbus-通道b,rtu-地址-线,3×115 v 400 hz线,gps-天线-信号,例如,rtu-地址-桥电路测试设备的RTU-脐带电缆的rtu-地址-线被桥接,以便要测试的导弹具有rtu-地址,即哪种模式与rtu-地址不同。
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