DEFSTAN 00-18(PT1)SEC4/3(1995) : 1995
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
AVIONICS DATA TRANSMISSION INTERFACE SYSTEMS - PART 1: GUIDE TO INTERFACE SYSTEMS - SECTION 4: GUIDE TO THE DISCRETE SIGNAL INTERFACES STANDARD
English
01-01-1995
02-11-2015
Chapter one. General
1 Scope and purpose
2 Background
3 Related documents
4 Design opportunities
5 Discrete signal use
Chapter two. Interpretation of the standard
0 General
Introduction
1 Scope
2 Discrete signal types
3 Purpose
4 Related documents
5 Definitions
General requirements
6 Test and operating requirements
7 Forms of signals
8 Interface categories and constraints
Critical timing signalling
9 General
10 Transmitter
11 Receiver
12 Cable
Non-critical timing signalling
13 General
14 Transmitter
15 Receiver
16 Cable
Low power switching
17 General
18 Low power switch
19 Switching loads
20 Cable
Fault detecting, non-critical timing signalling
interface
21 General
22 Switch element
23 Sensor element
24 Cable
25 Electromagnetic compatibility
Figure 1: Discrete interface for critical timing signalling
Figure 2: Transmitter test circuit
Figure 3: Transmitter waveforms for critical timing signalling
Figure 4: Receiver test circuit
Figure 5: Receiver waveform for critical timing signalling
Figure 6: Discrete interface for non-critical timing signalling
Figure 7: Transmitter waveforms for non-critical timing signalling
Figure 8: Receiver waveform for non-critical timing signalling
Figure 9: Low power switching interface
Figure 10: Discrete interface for fault detecting, non-critical
timing signalling
Figure 11: Switch element output waveforms
Figure 12: Sensor element operation
Figure 13: Example of interconnection of multiple sensor elements
Intended to provide users and potential users with an understanding of its background and characteristics and potential.
| DevelopmentNote |
Supersedes DEFSTAN 00-18(PT1)SEC4/2(1991) (06/2003) This standard is obsolescent because it is no longer required for procurement of new equipment but is retained for maintenance purposes in support of existing in-service equipment. (01/2011)
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| DocumentType |
Standard
|
| Pages |
46
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Withdrawn
|
| Supersedes |
| STANAG 3909 : 2017 | DISCRETE SIGNAL INTERFACES |
| AAVSP-04 : 2017 | DISCRETE SIGNAL INTERFACES |
| SAE ARP4258A | Application of Low Speed Avionic System Discrete Signal Interfaces |
| DEFSTAN 59-41(PT4)/3(1996) : 1996 | ELECTROMAGNETIC COMPATIBILITY - PART 4: LARGE EQUIPMENT TESTING |
| STANAG 3837 : 0 | AIRCRAFT STORES ELECTRICAL INTERCONNECTION SYSTEM |
| DEFSTAN 59-41(PT3)/5(1995) : 1995 | ELECTROMAGNETIC COMPATIBILITY - PART 3: TECHNICAL REQUIREMENTS TEST METHODS AND LIMITS |
| DEFSTAN 59-41(PT1)/7(2002) : 2002 | ELECTROMAGNETIC COMPATIBILITY - PART 1: INTRODUCTION AND GUIDE TO THE SPECIFICATION AND SELECTION OF EMC REQUIREMENTS |
| DEFSTAN 59-41(PT6)/1(1994) : 1994 | ELECTROMAGNETIC COMPATIBILITY - PART 6: CODE OF PRACTICE FOR MILITARY VEHICLES INSTALLATION GUIDELINES |
| DEFSTAN 00-18(PT2)/2(1990) : 1990 | AVIONIC DATA TRANSMISSION INTERFACE SYSTEMS - PART 2: SERIAL, TIME DIVISION, COMMAND/RESPONSE MULTIPLEX DATA BUS STANDARD |
| DEFSTAN 59-41(PT5)/3(2003) : 2003 | ELECTROMAGNETIC COMPATIBILITY - PART 5: PERFORMANCE SPECIFICATION FOR SPECIALISED EMC TEST EQUIPMENT |
| MIL R 39016/7 : F | RELAY, ELECTROMAGNETIC, ESTABLISHED RELIABILITY, SPDT, LOW LEVEL TO 1 AMPERE |
| DEFSTAN 59-41(PT7)/1(1995) : 1995 | ELECTROMAGNETIC COMPATIBILITY - PART 7: CODE OF PRACTICE FOR HM SHIPS INSTALLATION GUIDELINES |
| MIL-STD-1346 Revision C:1994 | RELAYS, SELECTION AND APPLICATION OF (NO S/S DOCUMENT) |
| STANAG 3909 : 2017 | DISCRETE SIGNAL INTERFACES |
| DEFSTAN 59-41(PT2)/5(2002) : 2002 | ELECTROMAGNETIC COMPATIBILITY - PART 2: MANAGEMENT AND PLANNING PROCEDURES |