SNU 84-1/F16 REV B CH 1 15JUL92

Inertial navigation unit

SNU 84-1/F16 REV B CH 1 15JUL92 Description

15.187 inches overall length, 7.625 inches overall height, 6.750 inches overall width, dc current type, F-16 a to d model aircraft end item identification.

Features

Receives 26 v, 400 hz single phase synchro reference power; aircraft 28 vdc discrete power excluding battery back up power and has critical application

Properties of SNU 84-1/F16 REV B CH 1 15JUL92

Overall Length:
15.187 inches
Overall Height:
7.625 inches
Overall Width:
6.750 inches
Current Type:
Dc
End Application:
F-16 a to d model aircraft
Criticality Code Justification:
Feat
Voltage In Volts:
115.0 and 200.0
Frequency In Hertz:
400.0
Functional Description:
5capable of determining position, velocity, heading, accelerations, body rates, and attitude in the autonomous mode from take off to landing after a ground alignment in the following modes: gyrocompass, stored heading, best available true heading
Supplementary Features:
Electrostatic discharge sensitive
NSN:
6605-01-319-6483
Description:
Inertial Navigation Unit
Cage Code:
81349

Definition Inertial Navigation Unit

A self-contained line replaceable unit that provides acceleration, velocity, position, and altitude for piloting and navigating an aircraft. It is part of an inertial navigation system and may contain an inertial refernce unit, navigation.

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Last modified 11/15/2024