6605-14-501-3317

Inertial Navigation System

6605145013317 145013317 43173003 4317-61

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

6605-14-501-3317 INERTIAL NAVIGATION SYSTEM 6605145013317 145013317

Managed by France
NSN Created on 29 Oct 1997
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
6605-14-501-3317 INERTIAL NAVIGATION SYSTEM 6605145013317 145013317 1/1
NSN 6605-14-501-3317 (Generic Image) 1/1

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43173003 4317-61 A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw
RQST NE Updated Every Day 6605-14-501-3317 RQST Updated Every Day 6605-14-501-3317 RQST NE Related Documents
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3110-15-070-1073 Annular Ball Bearing 3110150701073150701073 Bearing 3110150701073150701073 6605-14-501-3317
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ring turns upon 501-3317 DEMIL: | DEMILI : | CRITICALITY : | HMIC : | PMIC : | EDC: | ADPEC : 6605-14-501-3317
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DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

6605-14-501-3317 is a Inertial Navigation System

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France (ZF)

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