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&#59; to input data into an electronic system&#59; 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

7025-14-545-4821 TRACKBALL,DATA ENTRY 7025145454821 145454821

Managed by France
NSN Created on 13 Apr 2005
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
7025-14-545-4821 TRACKBALL,DATA ENTRY 7025145454821 145454821 1/1
NSN 7025-14-545-4821 (Generic Image) 1/1

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Data Entry Trackball 7025145454821 145454821 engine. https//www.nsnlookup.com /fsg-28/fsc-2840/
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.

7025-14-545-4821 Demil Restrictions 7025-14-545-4821

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7025-14-545-4821 is a Data Entry Trackball

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France (ZF)

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