890500-0011

Inertial navigation unit

890500-0011 Description

11.780 inches overall length, 6.530 inches overall height, 8.150 inches overall width, ac current type, inertial navigation system F-16, A-10, FB-111, C-130, RF4C, EF-111 aircraft end item identification.

Features

Mounting: hard mounted; material: aluminum alloy case; provides outputs of acceleration, velocity, position, heading, attitude (pitch and roll), attitude rates (pitch, roll, azimuth) and time, pitch and roll synchro (analog), baro inertial altitude (when provided with barometric altitude data); performs rapid reaction, sotred heading alignments, rapid reaction alignment of a degraded accuracy (attitued heading reference system) mode with outputs of heading, attitude, angular rate and acceleration

Properties of 890500-0011

Overall Length:
11.780 inches
Overall Height:
6.530 inches
Overall Width:
8.150 inches
Current Type:
Ac
End Application:
Inertial navigation system f-16, a-10, fb-111, c-130, rf4c, ef-111 aircraft
Voltage In Volts:
115.0 and 200.0
Phase:
Single
Frequency In Hertz:
400.0
Functional Description:
Provides a self contained fully automatic strapdown inertial reference for piloting and navigating an aircraft
Nuclear Hardness Critical Feature:
Hardened
Reference Data And Literature:
Tech order 5n1-4-23-14
NSN:
6605-01-357-8976
Description:
Inertial Navigation Unit
Cage Code:

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 10/07/2024