6605-14-576-6277

Inertial Navigation System

6605145766277 145766277 704A47133300 802715-0007

A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw and roll axis of land vehicle, watercraft or aircraft and calculates the distance from a reference point. They can include INERTIAL NAVIGATION UNIT(s); PLATFORM, INERTIAL; power supplies; subsystems; mode selectors; and control displays. View more Inertial Navigation System

6605-14-576-6277 INERTIAL NAVIGATION SYSTEM 6605145766277 145766277

Managed by France
NSN Created on 2 Jul 2013
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
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6605-14-576-6277 Inertial Navigation System 6605145766277
704A47133300 802715-0007 A self-contained, dead-reckoning system that senses acceleration along the
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6605-14-576-6277 is a Inertial Navigation System

6605-14-576-6277 End Users End Users 6605-14-576-6277

France (ZF)

6605-14-576-6277 Manufacturers Approved Sources 6605-14-576-6277

Part Number
Manufacturer
Status
704A47133300
F0210 - Airbus Helicopters (Ets De (Active)
Source Control
RNCC 1 RNVC 2 DAC 5
802715-0007
15280 - Northrop Grumman Systems Corporation (Replaced)
Original Design
RNCC 3 RNVC 9 DAC 4

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