CN-1694(V)4/ASN-172

Inertial navigation system

CN-1694(V)4/ASN-172 Description

F/A18-A/B gps end item identification, agav criticality code justification.

Properties of CN-1694(V)4/ASN-172

End Application:
F/a18-a/b gps
Criticality Code Justification:
Agav
NSN:
6605-01-428-9999
Description:
Inertial Navigation System
Cage Code:
72143

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 05/21/2024