MIL-STD-1553 Revision B:1978
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA
10-05-2021
1 Scope
1.1 Scope
1.2 Application
2 Referenced documents
2.1 Issue of documents
3 Definitions
3.1 Bit
3.2 Bit rate
3.3 Pulse Code Modulation (PCM)
3.4 Time Division Multiplexing (TDM)
3.5 Half duplex
3.6 Word
3.7 Message
3.8 Subsystem
3.9 Data bus
3.10 Terminal
3.11 Bus controller
3.12 Bus monitor
3.13 Remote Terminal (RT)
3.14 Asynchronous operation
3.15 Dynamic bus control
3.16 Command/response
3.17 Redundant data bus
3.18 Broadcast
3.19 Mode code
4 General requirements
4.1 Test and operating requirements
4.2 Data bus operation
4.3 Characteristics
4.3.1 Data form
4.3.2 Bit priority
4.3.3 Transmission method
4.4 Terminal operation
4.4.1 Common operation
4.4.2 Bus controller operation
4.4.3 Remote terminal
4.4.4 Bus monitor operation
4.5 Hardware characteristics
4.5.1 Data bus characteristics
4.5.2 Terminal characteristics
4.6 Redundant data bus requirements
4.6.1 Electrical isolation
4.6.2 Single event failures
4.6.3 Dual standby redundant data bus
5 Detail requirements
Figures
1 Sample multiplex data bus architecture
2 Data encoding
3 Word formats
4 Command and status sync
5 Data sync
6 Information transfer formats
7 Broadcast information transfer formats
8 Intermessage gap and response time
9 Data bus interface using trans. coupling
10 Data bus interface using direct coupling
11 Coupling transformer
12 Terminal I/O characteristics for transformer coupled
and direct coupled stubs
13 Output waveform
Tables
I Assigned mode codes
II Criteria for acceptance or rejection of a terminal
for the noise rejection test
Appendix
10 General
10.1 Redundancy
10.2 Bus controller
10.3 Multiplex selection criteria
10.4 High reliability requirements
10.5 Stubbing
10.6 Use of broadcast option
20 General
20.1 Mode codes
20.2 Broadcast command
20.3 Mode code indicators
20.3.1 Bus controllers
20.3.2 Remote terminals
20.4 Data bus cable
20.4.1 Shielding
20.4.2 Characteristic impedance
20.5 Cable coupling
20.6 Direct coupled stubs
20.7 Redundant data bus requirements
20.8 Design considerations
20.8.1 Mode code indicator
20.8.2 Clock stability
20.8.3 Response time
Appendix Figures
10.1 Illustration of possible redundancy
10.2 Illustration of possible redundancy
Describes digital, command response, time division multiplexing techniques on aircraft. Covers data bus line and interface electronics, defines operation and information flow on multiplex data bus and functional and electrical formats used. Coverage includes definitions, data bus operation, transmission method, data code, remote terminal address, optional mode control, electrical isolation, and output noise. Also gives tables, diagrams and appendices.
Committee |
FSC MCCR
|
DevelopmentNote |
Updated by SAE AS 1773 in part.
|
DocumentType |
Standard
|
Pages |
425
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
SupersededBy |
AFGS-87213 Revision B:1993 | DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
DEFSTAN 00-13/3(1994) : 1994 | REQUIREMENTS FOR THE ACHIEVEMENT OF TESTABILITY IN ELECTRONIC AND ALLIED EQUIPMENT |
MIL-R-29583 Base Document:1992 | RADIO SET |
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SAE AS 47643 : 2017 | VERIFICATION METHODS FOR MIL-STD-1760E AIRCRAFT STATION INTERFACES |
MIL-STD-7080 Base Document:1994 | SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT |
DEFSTAN 00-18(PT1)SEC1/2(1989) : 1989 | AVIONIC DATA TRANSMISSION INTERFACE SYSTEMS - PART 1: GUIDE TO INTERFACE SYSTEMS - SECTION 1: INTRODUCTION |
MIL-DTL-62421 Revision A:2009 | CONTROL, UNIT, ELECTRONIC, DIGITAL |
MIL-DTL-17-201 Revision A:2016 | CABLES, RADIO FREQUENCY, FLEXIBLE, TWINAXIAL, SINGLE SHIELD, DATA BUS, 77 OHMS |
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ANSI INCITS TR 42 : 2007 : R2017 | INFORMATION TECHNOLOGY - FIBRE CHANNEL - AVIONICS ENVIRONMENT - UPPER LAYER PROTOCOL (FC-AE-1553) |
ANSI INCITS TR 31 : 2002 : R2007 | FIBRE CHANNEL - AVIONICS ENVIRONMENT (FC-AE) |
ARINC 755-5 : 2018 | MULTI-MODE RECEIVER (MMR) - DIGITAL |
MIL D 87213 : 0 | DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-PRF-32098 Revision A:2004 | ULTRAFILTRATION SYSTEM, 10-GALLON PER MINUTE OILY WASTE MEMBRANE (OWMS-10) |
SAE AIR 6006 : 2009 | MODELING AND SIMULATION CAPABILITIES FOR AEROSPACE WDM LAN APPLICATIONS |
SAE AS 4290 : 2012 | VALIDATION TEST PLAN FOR AS 4074 LINEAR TOKEN PASSING MULTIPLEX DATA BUS |
SAE AS 15532 : 2016 | DATA WORD AND MESSAGE FORMATS |
ISO/IEC TR 14165-312:2009 | Information technology Fibre Channel Part 312: Avionics environment upper layer protocol MIL-STD-1553B Notice 2 (FC-AE-1553) |
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DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-R-81876 Revision B:1988 | RECEIVER, TRANSMITTER RADIO SET AN/APX-100(V) |
DEFSTAN 00-69(PT2)/1(1998) : 1998 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM - PART 2: DESIGN PRINCIPLES AND PRACTICES FOR, AND GUIDE TO, THE IMPLEMENTATION OF THE AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
AFGS-87219 Revision B:2012 | ELECTRICAL POWER SYSTEMS, AIRCRAFT |
MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
DEFSTAN 00-18(PT7)/2(1999) : 1999 | AVIONIC DATA TRANSMISSION INTERFACE SYSTEMS - PART 7: UTILITIES DATA BUS STANDARD |
SAE AS 4114 : 2017 | PRODUCTION TEST PLAN FOR THE TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS CONTROLLERS |
BS G 264:2005 | Specification for avionic data transmission interface systems. Utilities bus |
DEFSTAN 00-970(PT9)/5(2009) : 2009 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 9: UAV SYSTEMS |
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 |
MIL-STD-188 Revision C:1969 | MILITARY COMMUNICATIONS SYSTEM TECHNICAL STANDARDS |
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SAE AS 5609 : 2017 | AIRCRAFT/STORE COMMON INTERFACE CONTROL DOCUMENT FORMAT STANDARD |
SAE AIR 6027 : 2017 | CONSIDERATIONS FOR SAFE STORE OPERATION ON MANNED AND UNMANNED VEHICLES |
SAE ARP 94910 : 2012 | AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
ANSI INCITS TR 31 : 2002 | FIBRE CHANNEL - AVIONICS ENVIRONMENT (FC-AE) |
SAE AS 42701 : 2014 | VALIDATION METHODS FOR MIL-STD-1760D MISSION STORES |
SAE AS 4112 : 2017 | PRODUCTION TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS REMOTE TERMINALS |
SAE AS 1773 : 2018 | FIBER OPTICS MECHANIZATION OF A DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
SAE AS 5653 : 2014 | HIGH SPEED NETWORK FOR MIL-STD-1760 |
SAE AIR 5020 : 2012 | TIME-DEPENDENT IN-FLIGHT THRUST DETERMINATION |
DEFSTAN 00-18(PT2)/2(1990) : 1990 | AVIONIC DATA TRANSMISSION INTERFACE SYSTEMS - PART 2: SERIAL, TIME DIVISION, COMMAND/RESPONSE MULTIPLEX DATA BUS STANDARD |
SAE AIR 4013 : 2012 | MULTIPLEX DATA BUS NETWORKS FOR MIL-STD-1760 STORES |
DEFSTAN 66-31(PT1)/2(2008) : 2008 | BASIC REQUIREMENTS AND TESTS FOR ELECTRONIC AND ELECTRICAL TEST AND MEASUREMENT EQUIPMENT - PART 1: INTRODUCTION AND GUIDE TO THE SPECIFICATION AND SELECTION OF TEST AND MEASUREMENT EQUIPMENT BY THE PROCURING AUTHORITY |
MIL-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
DEFSTAN 00-18(PT1)SEC3/2(1990) : 1990 | AVIONIC DATA TRANSMISSION INTERFACE SYSTEMS - PART 1: GUIDE TO INTERFACE SYSTEMS - SECTION 3: GUIDE TO THE SIMPLEX AND HALF DUPLEX SERIAL DIGITAL TRANSMISSION INTERFACE SYSTEMS STANDARD |
MIL-C-85518 Base Document:1984 | COMPUTER SET, STANDARD AIRBORNE AN/AYK-14(V) GENERAL SPECIFICATION FOR |
DEFSTAN 00-18(PT1)SEC2/2(1991) : 1991 | AVIONIC DATA TRANSMISSION INTERFACE SYSTEMS - PART 1: GUIDE TO INTERFACE SYSTEMS - SEC 2: GUIDE TO THE SERIAL, TIME DIVISION, COMMAND/RESPONSE MULTIPLEX DATA BUS STANDARD |
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 |
MIL-R-87245 Base Document:1986 | RADIO COMMUNICATION SYSTEM, AIRBORNE (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA: ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
MIL-I-87216 Base Document:1984 | INSTRUMENT SYSTEMS, AIRBORNE REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT PATTERSON AFB OH 45433-6503 |
MIL C 85629 : A (1) | CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
MIL-DTL-17-176 Revision E:2015 | Cable, Radio Frequency, Flexible, Twin, M17/176-00002 and M17/176-00003 |
MIL-HDBK-2124 Base Document:2000 | FLIGHT DATA RECORDER FUNCTIONAL STANDARDS FOR |
DEFSTAN 66-31(PT1)/1(2007) : 2007 | BASIC REQUIREMENTS & TESTS FOR ELECTRONIC & ELECTRICAL TEST & MEASUREMENT EQUIPMENT - PART 1: INTRODUCTION AND GUIDE TO THE SPECIFICATION AND SELECTION OF TEST AND MEASUREMENT EQUIPMENT BY THE PROCURING AUTHORITY |
SAE AS 47641 : 2017 | VALIDATION METHODS FOR MIL-STD-1760B AIRCRAFT STATION INTERFACES |
SAE AS 5716 : 2012 | STANDARD ELECTRICAL AND LOGICAL INTERFACE FOR AIRBORNE FUZING SYSTEMS |
NASA HDBK 4001 : 0 | ELECTRICAL GROUNDING ARCHITECTURE FOR UNMANNED SPACECRAFT |
RE.AERO 74430 : 1990 | REPRESENTATION OF ELECTRICAL MASSES USED IN AIRCRAFT AND TEST INSTALLATIONS |
SAE AS 15531 : 2017 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
IEEE 1671.3-2007 | IEEE Standard for Automatic Test Markup Language (ATML) for Exchanging Automatic Test Information via XML (eXtensible Markup Language): Exchanging UUT (Unit Under Test) Description Information |
MIL-STD-1773 Base Document:1988 | FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
SAE JA 6268 : APR 2018 | DESIGN & RUN-TIME INFORMATION EXCHANGE FOR HEALTH-READY COMPONENTS |
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PREN 3716-002 : 200P1 | AEROSPACE SERIES - CONNECTORS, SINGLE-WAY WITH TRIAXIAL INTERFACE, FOR TRANSMISSION OF DIGITAL DATA - PART 002: CONDITIONS OF USE AND LIST OF PRODUCT STANDARDS |
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SAE AIR 6234 : 2016 | HANDBOOK: STANDARD ELECTRICAL AND LOGICAL INTERFACE FOR AIRBORNE FUZING SYSTEMS |
SAE AS 4115 : 2017 | TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS SYSTEM |
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EN 4660-003:2011 | Aerospace series - Modular and Open Avionics Architectures - Part 003: Communications/Network |
EN 3567-004:2001 | Aerospace series - In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B - Part 004: Double in-line couplers - Product standard |
MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
IEEE 1671.1-2009 | IEEE Standard for Automatic Test Markup Language (ATML) for Exchanging Automatic Test Equipment and Test Information via XML: Exchanging Test Descriptions |
MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
MIL-F-24259 Revision A:1987 | FLUID FLOWMETER, VOLUME VELOCITY TYPE |
PD 6526:1990 | Evaluation report on CIM architectures |
MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
MIL-HDBK-87213 Revision A:2005 | ELECTRONICALLY/OPTICALLY GENERATED AIRBORNE DISPLAYS |
IEEE DRAFT 896.10 : D4.0 JUL 95 | STANDARD FOR FUTUREBUS+ SPACEBORNE SYSTEMS PROFILE "S" |
DEFSTAN 00-18(PT7)/1(1999) : 1999 | AVIONIC DATA TRANSMISSION INTERFACE SYSTEMS - UTILITIES DATA BUS STANDARD |
MIL-STD-1397 Revision C:1995 | INPUT/OUTPUT INTERFACES, STANDARD DIGITAL DATA, NAVY SYSTEMS |
MIL-T-24664 Base Document:1986 | TEST SET, RADAR, AN/UPM-() |
SAE AIR 1873 : 2016 | GUIDE TO LIMITED ENGINE MONITORING SYSTEMS FOR AIRCRAFT GAS TURBINE ENGINES |
SAE AS 4270 : 2017 | VALIDATION METHODS FOR MIL-STD-1760 MISSION STORES |
SAE AS 4764 : 2017 | VALIDATION METHODS FOR MIL-STD-1760 AIRCRAFT STATION INTERFACES |
ANSI INCITS TR 42 : 2007 | INFORMATION TECHNOLOGY - FIBRE CHANNEL - AVIONICS ENVIRONMENT - UPPER LAYER PROTOCOL (FC-AE-1553) |
SAE AS 5652 : 2018 | 10 MEGABIT/SEC NETWORK CONFIGURATION DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
SAE AS 4113 : 2017 | VALIDATION TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS BUS CONTROLLERS |
SAE AS 47642 : 2017 | VALIDATION METHODS FOR MIL-STD-1760C AIRCRAFT STATION INTERFACES |
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SAE AS 4111 : 2017 | VALIDATION TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS REMOTE TERMINALS |
SAE AS 94900 : 2007 | AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
BS EN 4660-003:2011 | Aerospace series. Modular and open avionics architectures Communications/Network |
BS EN 3716-002:2006 | Aerospace series. Connectors, single-way, with triaxial interface, for transmission of digital data Conditions of use and list of product standards |
BS EN 3567-001:2001 | Aerospace series. In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B Technical specification |
BS EN 3567-003:2001 | Aerospace series. In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B Single in-line couplers. Product standard |
EN 16603-50-13:2014 | Space engineering - Interface and communication protocol for MIL-STD-1553B data bus onboard spacecraft |
EN 3567-003:2001 | Aerospace series - In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B - Part 003: Single in-line couplers - Product standard |
EN 3716-002:2006 | Aerospace series - Connectors, single-way with triaxial interface, for transmission of digital data - Part 002: Conditions of use and list of product standards |
MIL A 87211 : NOTICE 1 | AIR DATA SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD ENES, WRIGHT PATTERSON, AFB OH 45433 6503 |
DOD STD 1788 : LATEST | AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
SAE AS 4116 : 2017 | TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS BUS MONITORS |
MIL-F-24701 Base Document:1988 | FLOWMETER, LIQUID, ULTRASONIC, NON-INTRUSIVE |
BS EN 16603-50-13:2014 | Space engineering. Interface and communication protocol for MIL-STD-1553B data bus onboard spacecraft |
SAE ARP 4729 : 2017 | DOCUMENT FOR 270 VOLTAGE DIRECT CURRENT (270 V DC) SYSTEM |
SAE AS 50881 : 2015 | WIRING AEROSPACE VEHICLE |
MIL-PRF-32007 Base Document:2003 | OILY WASTEWATER SEPARATION SYSTEM, 6.7-GALLON PER MINUTE NAVY INTEGRATED MEMBRANE SYSTEM (NIMS) |
MIL-C-81883 Base Document:1976 | CONTROL GROUP, ELECTRIC POWER OK-XXX (V) A GENERAL SPECIFICATION FOR |
MIL-STD-1293 Base Document:1979 | ELECTRO-MECHANICAL COMMAND INSTRUMENT SYSTEM FOR ROTARY WING AIRCRAFT |
PREN 4660-003 : 200P1 | AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 003: FINAL DRAFT OF PROPOSED STANDARDS FOR COMMUNICATIONS/NETWORK |
PREN 3910-001 : 200P1 | AEROSPACE SERIES - HIGH SPEED DATA TRANSMISSION UNDER STANAG 3838 OR FIBRE OPTIC EQUIVALENT CONTROL |
DEFSTAN 00-18(PT1)SEC2/1(1982) : 1982 AMD 3 1987 | AVIONIC DATA TRANSMISSION INTERFACE SYSTEMS SEC 2 GUIDE TO THE SERIAL, TIME DIVISION, COMMAND RESPONSE MULTIPLEX DATA BUS STANDARD. |
SAE ARP 5584 : 2011 | DOCUMENT FOR ELECTRIC POWER MANAGEMENT |
AEDP-6 : 2014 | NATO ADVANCED DATA STORAGE INTERFACE REQUIREMENTS AND IMPLEMENTATION GUIDE |
I.S. EN 4660-003:2011 | AEROSPACE SERIES - MODULAR AND OPEN AVIONICS ARCHITECTURES - PART 003: COMMUNICATIONS/NETWORK |
SAE AIR 5683 : 2016 | HIGH PERFORMANCE 1553 RESEARCH AND DEVELOPMENT |
BS EN 3567-004:2001 | Aerospace series. In-line couplers for use in multiplex data bus systems in accordance with MIL-STD-1553B Double in-line couplers. Product standard |
MIL-E-6051 Revision D:1967 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS, SYSTEM |
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