0.8 nmi/hr free inertial; pseudorange and delta range mechnization; 1553 b and analog i/o; 5-channel ca/p (y) code receiver; full sa-as capabilities; l1/l2 capabilities; 0.6 in. Single pitch module; 10 meter cep gps/inertial; 0.01 meters/sec (rms) velocity per axis; 0.02 degrees (rms) attitude
A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw and roll axis of the aircraft and calculates the distance traveled from a reference point. They can include inertial navigation unit(s);platform, inertial; power supplies; subsystems; mode selectors; and control displays.
Classification: Parts & accessories for direction finding compasses and other navigational instruments and appliances
NSN 6645-01-053-3185
NSN 6685-01-478-1771
NSN 6320-00-937-5625
NSN 7035-01-265-2301
NSN 5945-01-388-1997
NSN 5998-01-221-8609
NSN 6220-01-333-4733
NSN 7035-01-058-1935
NSN 5935-00-252-1800
NSN 5905-01-147-3855
NSN 5960-01-406-4136
NSN 7035-01-465-0391