6605-14-564-9781
Inertial Navigation System
6605145649781 145649781 704A47133284 8025711SLO
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
Managed by France
NSN Created on 24 Jun 2010
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 6605-14-564-9781
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704A47133284 8025711SLO A self-contained, dead-reckoning system that senses acceleration along the pitch
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RQST NE Updated Every Day 6605-14-564-9781 RQST Updated Every Day 6605-14-564-9781 RQST NE Related Documents
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Restrictions 6605-14-564-9781
End Users 6605-14-564-9781
- France (ZF)
Approved Sources 6605-14-564-9781
- Part Number
- Manufacturer
- Status
- 704A47133284
- Manufacturer
- F0210 - Airbus Helicopters (Ets De (Active)
- Source Control
- Source Control
- 8025711SLO
- 26916 - Northrop Grumman Systems Corporation (Active)
- Primary Buy
- Primary Buy
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