CG1135AC01

Inertial navigation system

CG1135AC01 Description

Inertial system navigation , lg. 6.630 in; h 4.500 in; w 5.750 in; operating temperature minus 15 deg c to plus 48 deg c; power 28 vdc .

Features

Lg. 6.630 in; h 4.500 in; w 5.750 in; operating temperature minus 15 degrees c to plus 48 degrees c; power 28 vdc

Properties of CG1135AC01

Part Name Assigned By Controlling Agency:
Inertial system navigation
NSN:
6605-01-323-4368
Description:
Inertial Navigation System
Cage Code:
94580

Definition Inertial Navigation System

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.

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Last modified 05/01/2024