6605-14-511-5482
Inertial Navigation System
6605145115482 145115482 704A47-133-247 C17008DA01
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 Dec 1998
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 6605-14-511-5482
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Related Documents 6605-14-511-5482 1+ Documents (More...)
704A47-133-247 C17008DA01 A self-contained, dead-reckoning system that senses acceleration along the
RQST NE Updated Every Day 6605-14-511-5482 RQST Updated Every Day 6605-14-511-5482 RQST NE Related Documents
6605-14-511-5482 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-66/fsc-6605/fr 6605-14-511-5482
RQST NE Updated Every Day 6605-14-511-5482 RQST Updated Every Day 6605-14-511-5482 RQST NE Related Documents
6605-14-511-5482 1+ Documents ( More... ) https//www.nsnlookup.com /fsg-66/fsc-6605/fr 6605-14-511-5482
Restrictions 6605-14-511-5482
End Users 6605-14-511-5482
- Brazil (YA)
- France (ZF)
- Netherlands (ZN)
Approved Sources 6605-14-511-5482
- Part Number
- Manufacturer
- Status
- 704A47-133-247
- Manufacturer
- F0210 - Airbus Helicopters (Ets De (Active)
- Source Control
- Source Control
- C17008DA01
- F9111 - Thales Avs France Sas (Active)
- Primary Buy
- Primary Buy
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