34209400-TB44-020

Inertial navigation system

34209400-TB44-020 Description

11.280 inches overall depth, 7.700 inches overall height, 16.800 inches overall width, dc current type, electronic actuation method.

Features

Contains 3 ring laser gyros and 3 accelerometers; includes provisions for internal battery; max current 5 amps; 52 lbs; rack mounted into a mounting bracket on guide pins and swing blots

Properties of 34209400-TB44-020

Overall Depth:
11.280 inches
Overall Height:
7.700 inches
Overall Width:
16.800 inches
Current Type:
Dc
Actuation Method:
Electronic
End Application:
F/a-18 aircraft
Electrical Connection Quantity:
5
Mounting Point Quantity:
2
Part Name Assigned By Controlling Agency:
Inertial navigation unit
Voltage In Volts:
28.0
Functional Classification:
Oo-2.2
Functional Description:
Measures translational and angular motion which is converted in various coordinate axes and used to indicate platform position, velocity, acceleration, attitude, angular motion, and time
Entry Date:
11-02-15
NSN:
6605-01-591-9321
Description:
Inertial Navigation System
Cage Code:
0BFA5

Definition Inertial Navigation System

A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw and roll axis of the aircraft and calculates the distance traveled from a reference point. They can include inertial navigation unit(s);platform, inertial; power supplies; subsystems; mode selectors; and control displays.

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Last modified 05/06/2024