An electromechanical and/or electronic, self-contained, automatically controlling device. It is designed to be mounted on the body or contained within the guidance section of an air launched missile. Its funtion is to measure linear acceleration, angular rate, delta-velocity and delta-altitude. It contains sensors, accelerometers, gyroscopes and the like. Excludes inertial navication system.
Classification: Parts for guided missiles
NSN 6150-01-472-9882
NSN 6150-00-753-3950
NSN 5915-00-528-9286
NSN 5998-00-581-3867
NSN 5999-01-175-0287
NSN 5975-01-357-7440
NSN 5905-01-337-2907
NSN 7035-00-153-3826
NSN 5910-01-413-4420
NSN 5985-01-357-7200
NSN 6150-01-449-8114
NSN 6220-01-308-3918