• 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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA

    Available format(s):  PDF

    Superseded date:  10-05-2021

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Table of Contents - (Show below) - (Hide below)

    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

    Abstract - (Show below) - (Hide below)

    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.

    General Product Information - (Show below) - (Hide below)

    Committee FSC MCCR
    Development Note Updated by SAE AS 1773 in part.
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    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
    SAE AS 4117 : 2017 TEST PLAN FOR THE DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS COUPLERS, TERMINATORS, AND DATA BUS CABLES
    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
    MIL-STD-2124 Revision A:1984 FLIGHT INCIDENT RECORDER/CRASH POSITION LOCATOR, MINIMUM PERFORMANCE STANDARDS FOR
    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)
    DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
    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
    SAE AIR5691A : 2017 GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY INDICATING SYSTEMS
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    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
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    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
    DEFSTAN 59-71(PT2)/1(1993) : 1993 CRIMPED ELECTRICAL CONNECTORS FOR COPPER CONDUCTORS - PART 2: SPECIALISED CRIMPING PROCESSES
    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
    SAE AS 5395:2006 HEALTH AND USAGE MONITORING SYSTEM DATA INTERCHANGE SPECIFICATION
    SAE AS 5658 A : 2016 PLATFORM/SUBSYSTEM COMMON INTERFACE CONTROL DOCUMENT FORMAT
    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
    NASA MSFC STD 3012 : 2012 ELECTRICAL, ELECTRONIC, AND ELECTROMECHANICAL (EEE) PARTS MANAGEMENT AND CONTROL REQUIREMENTS FOR MSFC SPACE FLIGHT HARDWARE
    EN 3567-001 : 2001 AEROSPACE SERIES - IN-LINE COUPLERS FOR USE IN MULTIPLEX DATA BUS SYSTEMS IN ACCORDANCE WITH MIL-STD-1553B - PART 001: TECHNICAL SPECIFICATION
    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
    NASA CCSDS 901.0-G : ISSUE 1 SPACE COMMUNICATIONS CROSS SUPPORT - ARCHITECTURE DESCRIPTION DOCUMENT
    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
    I.S. EN 16603-50-13:2014 SPACE ENGINEERING - INTERFACE AND COMMUNICATION PROTOCOL FOR MIL-STD-1553B DATA BUS ONBOARD SPACECRAFT
    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
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    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
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    DOD STD 1788 : LATEST AVIONICS INTERFACE DESIGN STANDARD (METRIC)
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    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
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    PREN 3910-001 : 200P1 AEROSPACE SERIES - HIGH SPEED DATA TRANSMISSION UNDER STANAG 3838 OR FIBRE OPTIC EQUIVALENT CONTROL
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