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MIL-STD-1553 Revision B:1978

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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

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PDF

Superseded date

10-05-2021

€17.95
Excluding VAT

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
SAE AS4117A Test Plan for The Digital Time Division Command/Response Multiplex Data Bus Couplers, Terminators, and Data Bus Cables
SAE AS47643 Verification Methods for MIL-STD-1760E Aircraft Station Interfaces
MIL-STD-7080 Base Document:1994 SELECTION & INSTALLATION OF AIRCRAFT ELECTRIC EQUIPMENT
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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)
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SAE AS15532A 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
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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 AS4114A Production Test Plan for the Time Division Command/Response Multiplex Data Bus 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 Guidance for the Design and Installation of Fuel Quantity Indicating Systems
SAE AS5609A Aircraft/Store Common Interface Control Document Format Standard
SAE AIR6027A Considerations for Safe Store Operation on Manned and Unmanned Vehicles
SAE ARP94910 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 AS42701 Validation Methods For MIL-STD-1760D Mission Stores
SAE AS4112A Production Test Plan for the Digital Time Division Command/Response Multiplex Data Bus Remote Terminals
SAE AS1773A Fiber Optics Mechanization of a Digital Time Division Command/Response Multiplex Data Bus
SAE AS5653B High Speed Network for MIL-STD-1760
SAE AIR5020A 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 AIR4013C 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 AS47641A Validation Methods for MIL-STD-1760B Aircraft Station Interfaces
SAE AS5716A 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 AS15531A 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 JA6268_201804 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 AS5658A Platform/Subsystem Common Interface Control Document Format
SAE AIR6234 Handbook: Standard Electrical and Logical Interface for Airborne Fuzing Systems
SAE AS4115A 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
MIL-T-24664 Base Document:1986 TEST SET, RADAR, AN/UPM-()
SAE AIR1873A Guide to Limited Engine Monitoring Systems for Aircraft Gas Turbine Engines
SAE AS4270A Validation Methods for MIL-STD-1760 Mission Stores
SAE AS4764A 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 AS5652A 10 Megabit/sec Network Configuration Digital Time Division Command/Response Multiplex Data Bus
SAE AS4113A Validation Test Plan for the Digital Time Division Command/Response Multiplex Data Bus Bus Controllers
SAE AS47642B 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 AS4111A Validation Test Plan for the Digital Time Division Command/Response Multiplex Data Bus Remote Terminals
SAE AS94900 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 AS4116A 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 ARP4729A Document for 270 Voltage Direct Current (270 V DC) System
SAE AS50881F 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 ARP5584 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 AIR5683A 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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