7025-14-545-4821
Data Entry Trackball
7025145454821 145454821 47222840
A device which includes a sphere mounted in a small open-topped box. The sphere is hand-operated by rotating it in a backward, a forward, or a sideway direction while maintaining the device in a fixed location. The movement of the sphere generates a signal which may be used to move a cursor and/or tracking symbol on the face of a display, such as a cathode ray tube; to input data into an electronic system; and/or to control the operation of a system. It may or may not include additional input devices, such as switches or variable resistors. View more Data Entry Trackball
Managed by France
NSN Created on 13 Apr 2005
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 7025-14-545-4821
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2840-01-485-5156 2840014855156 014855156 is a rigid item designed to help direct the flow of hot gases from an afterburner,turbine engine. it is an integral part of a nozzle,augmentor exhaust, aircraft gas turbine engine. the item is to the rear of and hinged to an augmentor nozzle section,convergent, aircraft gas turbine engine.
2840-01-485-1558 2840014851558 014851558 is a rigid item designed to help direct the flow of hot gases from an afterburner,turbine engine. it is an integral part of a nozzle,augmentor exhaust, aircraft gas turbine engine. the item is to the rear of and hinged to an augmentor nozzle section,convergent, aircraft gas turbine engine.
2840-01-515-4722 2840015154722 015154722 is a rigid item designed to help direct the flow of hot gases from an afterburner,turbine engine. it is an integral part of a nozzle,augmentor exhaust, aircraft gas turbine engine. the item is to the rear of and hinged to an augmentor nozzle section,convergent, aircraft gas turbine engine.
2840-01-485-5197 2840014855197 014855197 is a rigid item designed to help direct the flow of hot gases from an afterburner,turbine engine. it is an integral part of a nozzle,augmentor exhaust, aircraft gas turbine engine. the item is to the rear of and hinged to an augmentor nozzle section,convergent, aircraft gas turbine engine.
Restrictions 7025-14-545-4821
End Users 7025-14-545-4821
- France (ZF)
Approved Sources 7025-14-545-4821
- Part Number
- Manufacturer
- Status
- 47222840
- Manufacturer
- F0052 - Thales Dms France Sas (Active)
- Primary Buy
- Primary Buy
NATO Stock Numbers Related to 7025-14-545-4821
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