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 5930-01-472-0321
NSN 6650-01-479-5075
NSN 5895-01-068-0613
NSN 6685-01-605-3617
NSN 5920-01-599-8622
NSN 6150-01-280-5362
NSN 5950-00-852-5678
NSN 5935-00-083-5146
NSN 6145-00-432-7431
NSN 2925-01-100-3694
NSN 5985-01-182-2890
NSN 5965-00-144-2543