1420-12-378-8485
Guided Missile Fin
1420123788485 123788485 D0116448 D0116448-001
A movable airfoil, forming a part and/or all of the main directional control surfaces of a missile. It is usually perpendicular or approximately perpendicular to the longitudinal axis of the missile. Its function is to maintain uniformity of direction and to aid in the control of yaw, pitch, and roll of a guided missile in flight. View more Guided Missile Fin
Managed by Germany
NSN Created on 19 May 2009
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality

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Related Documents 1420-12-378-8485 2+ Documents (More...)
D0116448 D0116448-001 A movable airfoil, forming a part and/or all of the main directional control surfaces
RQST NE Updated Every Day 1420-12-378-8485 RQST Updated Every Day 1420-12-378-8485 RQST NE Related Documents
: 1420-12-378-8485 is a Guided Missile Fin End Users 1420-12-378-8485 Germany (ZG) Approved Sources
RQST NE Updated Every Day 1420-12-378-8485 RQST Updated Every Day 1420-12-378-8485 RQST NE Related Documents
: 1420-12-378-8485 is a Guided Missile Fin End Users 1420-12-378-8485 Germany (ZG) Approved Sources
1420-12-165-6288 Halter 0307161-10300-06RNCC: 5 | RNVC: 9 | DAC: 1 9 Jun 1976 1420-12-005-0708 1420-12-378-8485
Restrictions 1420-12-378-8485
End Users 1420-12-378-8485
- Germany (ZG)
Approved Sources 1420-12-378-8485
- Part Number
- Manufacturer
- Status
- D0116448
- Manufacturer
- D0078 - Diehl Defence Gmbh & Co. Kg (Active)
- Primary Buy
- Primary Buy
- D0116448-001
- D0078 - Diehl Defence Gmbh & Co. Kg (Active)
- Secondary Buy
- Secondary Buy
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