PREN 3910-001 : 200P1
Current
The latest, up-to-date edition.
AEROSPACE SERIES - HIGH SPEED DATA TRANSMISSION UNDER STANAG 3838 OR FIBRE OPTIC EQUIVALENT CONTROL
Hardcopy , PDF
English
31-01-1996
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0 Introduction
1 Scope
2 References
3 Definitions
4 General requirements
Annex A (informative) Specific Implementations
Annex B (informative) HS Fibre Optic Media Slash Sheets
Annex C (normative) Frame Check Sequence Implementation
Annex D (informative) Block Diagram for Error Rate/Waveform
Test
Annex E (informative) HS Electrical Media Slash Sheets
Annex F (informative) Block Diagrams for Electrical HS Bus
Error Rate Testing
Annex G (informative) Keyword Index
Specifies characteristics and requirements of a data bus system which consists of one or more High Speed (HS) Channel(s) for HS data transmission and one Low Speed (LS) Channel for control and LS data transmission. Defines the HS fibre optic or HS electrical data bus transmission line.
| Committee |
C2
|
| DevelopmentNote |
Supersedes PREN 3910. (08/2003)
|
| DocumentType |
Draft
|
| Pages |
91
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Current
|
| Supersedes |
| Standards | Relationship |
| DIN EN 3910-001:1996-06 (Draft) | Identical |
| PREN 3758 : 200P1 | AEROSPACE SERIES - SIMPLEX HIGH SPEED DATA TRANSMISSION SYSTEM |
| STANAG 3838 : 2016 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
| STANAG 3910 : 0 | HIGH SPEED DATA TRANSMISSION UNDER STANAG 3838 AVS OR FIBRE OPTIC EQUIVALENT CONTROL |
| MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
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