Special Features:

Hermetically sealed; contains no moving parts or gaseous cavities; 3 solid state fiber optic gyros and silicon accelerometers; operating temperature -54/+71 degrees c continuous operation

Properties:

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.