34249950-RN14-960

Inertial navigation system

34249950-RN14-960 Description

11.000 inches overall height, 8.500 inches overall width, CN-1689 end item identification, a) provides outputs of: acceleration, velocity, position, heading, attitude, attitude rates (roll, pitch, azimuth) b) contains 3 ring laser gyros .

Features

A) provides outputs of: acceleration, velocity, position, heading, attitude, attitude rates (roll, pitch, azimuth) b) contains 3 ring laser gyros and 3 accelerometers in a strapdown configuration c) embedded global positioning system receiver (egr) (rf input)- gasr based d) 1553/b multiplex bus compatible e) built in test incorporated f) 32 bit microprocessor g) arinc 429 interface card h) multi-mode receiver that provides: instrument landing system (ils), very high omni bearing receiver (vor), marker beacon (mb).

Properties of 34249950-RN14-960

Overall Height:
11.000 inches
Overall Width:
8.500 inches
End Application:
Cn-1689
NSN:
6605-01-532-6526
Description:
Inertial Navigation System
Cage Code:

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 05/21/2024