CN-1689(V)15/ASN

Inertial navigation unit

CN-1689(V)15/ASN Description

11.000 inches overall depth, 7.000 inches overall length, 7.000 inches overall height, dc current type, F-15 aircraft end item identification.

Features

Contains 3 ring laser gyros; 3 accelerometers in a strap down configuration, embedded global postion reciever, 1553/b mutiplex bus, built in test, f-15 avionics interface card

Properties of CN-1689(V)15/ASN

Overall Depth:
11.000 inches
Overall Length:
7.000 inches
Overall Height:
7.000 inches
Current Type:
Dc
End Application:
F-15 aircraft
Mounting Method:
Bolt clamp
Part Name Assigned By Controlling Agency:
Navigation unit, inertial-satellite signals
Voltage In Volts:
28.0
Functional Description:
F15 saasm embedded gps/ins (egi) unit is a self contained all-attitude line replaceable navigation unit. Povides the following outputs: acceleration, attitude (azimuth, pitch, roll), attitude rates and universal time coordinated. Provides inertial, blended & gps only position solutions
Reference Data And Literature:
Ddform61
Type/model Designation:
Cn-168 (v) 15/asn
NSN:
6605-01-511-3424
Description:
Inertial Navigation Unit
Cage Code:
80058

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 05/26/2024