HG1700AG73

Inertial navigation system

HG1700AG73 Description

2.900 inches overall height, dc current type, 3.700 inches overall diameter, P5CTS end item identification, ring mounting method.

Features

Mounting ring diameter 5.0 in.; +/- 15v DC , +/- 5v DC input voltages; hermetically sealed; unit weight approx. 1.6 lb.; output data rate 100hz/600hz; gyro input range +/- 1000 deg/sec; gyro rate scale factor 150 ppm; accelerometer range +/- 50 g; accelerometer lineari type 500 ppm; accelerometer scale 300 ppm; programmable, expandable serial i/o with rs422 interface

Properties of HG1700AG73

Overall Height:
2.900 inches
Current Type:
Dc
Overall Diameter:
3.700 inches
End Application:
P5cts
Mounting Method:
Ring
Part Name Assigned By Controlling Agency:
Inertial measurement unit, 3 deg.
NSN:
6605-01-536-9218
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 04/28/2024