K160A058-23

Inertial navigation unit

K160A058-23 Description

18.100 inches overall length, 7.900 inches overall height, 7.900 inches overall width, ac current type, AN/ASQ-184, B-1B aircraft end item identification.

Features

Additional power 28 vdc; roll 876.5 lbs square inch, yaw 953.4 lbs square inch, pitch 245.5 lbs square inch

Properties of K160A058-23

Overall Length:
18.100 inches
Overall Height:
7.900 inches
Overall Width:
7.900 inches
Current Type:
Ac
End Application:
An/asq-184, b-1b aircraft
Voltage In Volts:
26.0 and 115.0
Frequency In Hertz:
400.0
Functional Description:
Prime sensor for aircraft velocity, delta velocity, attitude and heading info. And provides all functions necessary for inertial navigation including self-contained alignment and generation of present position data; primary input/output interface is mil-std-1553b mux bus which permits communication with an avionics processor (ap)
NSN:
6605-01-252-9480
Description:
Inertial Navigation Unit
Cage Code:
88818

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 05/06/2024