34200650-30Q7

Inertial navigation system

34200650-30Q7 Description

Dc current type, 34200650-30Q7, egi ins system end item identification, 28.0 voltage in volts, angular rate, roll, pitch, YAW-420 deg/sec passive cooling per 40 watts ; neg 54 to pos 71 deg c .

Features

Angular rate, roll, pitch, yaw-420 deg/sec; passive cooling per 40 watts ; neg 54 to pos 71 degrees c

Properties of 34200650-30Q7

Current Type:
Dc
End Application:
34200650-30q7, egi ins system
Voltage In Volts:
28.0
NSN:
6605-01-487-8451
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 04/27/2024