STANAG 3910 : 0
Withdrawn
HIGH SPEED DATA TRANSMISSION UNDER STANAG 3838 AVS OR FIBRE OPTIC EQUIVALENT CONTROL
English
07-23-2013
Agreement to achieve easier development, improved maintenance and a decrease in life cycle costs of avionics systems by using standardized characteristics and requirements for an aircraft internal time division multiplex data bus for use in systems integration of aircraft sub-systems, consisting STANAG 3838 controlled fibre optic or electrical interconnection channel for high speed data transmission, the pre-European Norm 3910 (pre EN 3910).
| DocumentType |
Standard
|
| Pages |
8
|
| PublisherName |
NATO
|
| Status |
Withdrawn
|
| DEFSTAN 66-031(PT8)/2(2016) : 2016 | REQUIREMENTS FOR ELECTRONIC AND ELECTRICAL TEST AND MEASUREMENT EQUIPMENT - PART 8: REQUIREMENTS FOR AUTOMATIC TEST SYSTEMS UTILISING AN OPEN SYSTEM ARCHITECTURE |
| DEFSTAN 00-18(PT1)SEC5/2(1991) : 1991 | AVIONIC DATA TRANSMISSION INTERFACE SYSTEMS - PART 1: GUIDE TO INTERFACE SYSTEMS - SEC 5: GUIDE TO FIBRE OPTIC INTERFACE STANDARDIZATION |
| PREN 3910-001 : 200P1 | AEROSPACE SERIES - HIGH SPEED DATA TRANSMISSION UNDER STANAG 3838 OR FIBRE OPTIC EQUIVALENT CONTROL |
| STANAG 3838 : 2016 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
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