311875-2N12

Inertial navigation system

311875-2N12 Description

Any acceptable actuation method, hermetically sealed; contains no moving parts or gaseous cavities; 3 solid state fiber optic gyros .

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 of 311875-2N12

Actuation Method:
Any acceptable
Mounting Point Quantity:
4
NSN:
6605-01-483-9184
Description:
Inertial Navigation System
Cage Code:
06481

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 05/04/2024