V-36-3756-01

Inertial system navigatio sensor

V-36-3756-01 Description

Dc current type, any acceptable actuation method, 5 contact quantity, 1 electrical connection quantity, hole mounting method, gallium arsenic ir diode, silicon planar phototransistor. .

Features

Gallium arsenide ir diode, silicon planar phototransistor.

Properties of V-36-3756-01

Current Type:
Dc
Actuation Method:
Any acceptable
Contact Quantity:
5
Electrical Connection Quantity:
1
Mounting Method:
Hole
Mounting Point Quantity:
2
NSN:
6605-01-432-5873
Description:
Sensor,inertial System Navigatio
Cage Code:

Definition Inertial System Navigatio Sensor

A device designed to provide digital outputs of aircraft altitude, true heading, angular rates and accelerations, inertial velocity and acceleration, body rates and accelerations and aircraft position to associated avionics.

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Last modified 11/05/2024