CN-1689(V)9/ASN

Inertial navigation unit

CN-1689(V)9/ASN Description

9.800 inches overall depth, 7.000 inches overall height, 7.000 inches overall width, dc current type, C/KC-135 aircraft end item identification.

Features

2/3a c-cell gps battery installed; front connector panel: built in test; electrostatic discharge sensitive

Properties of CN-1689(V)9/ASN

Overall Depth:
9.800 inches
Overall Height:
7.000 inches
Overall Width:
7.000 inches
Current Type:
Dc
End Application:
C/kc-135 aircraft
Mounting Method:
Fixed flange
Part Name Assigned By Controlling Agency:
Navigation unit, inertial-satelite signals
Voltage In Volts:
28.0
Functional Description:
Embedded gps/ins (egi) unit is a self-contained all-attitude navigation line replaceable unit providing outputs of acceleration, attitude (azimuth, pitch, roll), attitude rates, heading, position, velocity, associated time tag information, and universal time coordinated (utc) synchronized time via externally controlled mil-std-1553b dual multiplex data bus which requests data & transmits updated data based upon the requirements of the interfacing avionics sysetems. Egi provides simultaneous ins only, blended gps/ins & gps only position solutions.
Reference Data And Literature:
Dd form 61
Relationship To Similar Equipment:
5 channel vs 12 channel p/n 34209200-40h4
Supplementary Features:
Contains 3 ring laser gyros and 3 accelerometers in a strap down configuration, embeded global positioning system reciever
Type/model Designation:
Cn-168 (v) 9/asn
NSN:
6605-01-426-8522
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 04/27/2024