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MIL-STD-1760 Revision E:2007
Current
The latest, up-to-date edition.
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AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
English
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. NOTES
APPENDIX A - Additional Interface Requirements
for GPS RF Signals
APPENDIX B - Data Bus Communication Rules and
Message Requirements
APPENDIX C - MIL-STD-1553 Data Bus Communication
Rules and Message Requirements
APPENDIX D - Fibre Channel Data Bus Communication
Rules and Message Requirements
APPENDIX E - Annotations Explaining Differences from
Revision D
Describes implementation requirements for the Aircraft/Store Electrical (and fiber optic) Interconnection System (AEIS) in aircraft and stores and provides a common interfacing capability for the operation and employment of stores on aircraft.
Committee |
AREA SESS
|
DocumentType |
Standard
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Pages |
219
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PublisherName |
US Military Specs/Standards/Handbooks
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Status |
Current
|
DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
SAE AIR 6114 : 2016 | INTERFACE FOR MICRO MUNITION (IMM) HANDBOOK |
MIL-STD-2156 Base Document:1983 | LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
MIL-STD-8591 Base Document:2005 | AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE) |
DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 07-085(PT1)/4(2017) : 2017 | DESIGN REQUIREMENTS FOR WEAPONS AND ASSOCIATED SYSTEMS - PART 1: MANDATORY DESIGN REQUIREMENTS |
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)/14(2014) : 2014 | 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)/11(2013) : 2013 | 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)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-STD-1353 Revision C:2014 | ELECTRICAL CONNECTORS, PLUG-IN SOCKETS AND ASSOCIATED HARDWARE, SELECTION AND USE OF |
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)/8(2011) : 2011 | 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 |
DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-DTL-2726 Revision C:2006 | Receptacle, Receptacle Plugs, Switch and Receptacles, and Outlets (Electrical), General Specification for |
DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
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 |
MIL-HDBK-244 Revision A:1990 | GUIDE TO AIRCRAFT - STORES COMPATIBILITY |
MIL-DTL-83538-1 Revision D:2008 | CONNECTORS AND ACCESSORIES, ELECTRICAL, CIRCULAR, UMBILICAL, RECEPTACLE, STORE ASSEMBLY, REMOVABLE CRIMP CONTACTS, SOCKETS, FOR MIL-STD-1760 APPLICATIONS (METRIC) |
DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
MIL STD 1763 : A | AIRCRAFT STORES CERTIFICATION PROCEDURES |
MIL-DTL-83538-9 Revision B:2008 | CONNECTORS AND ACCESSORIES, ELECTRICAL, CIRCULAR, UMBILICAL, ADAPTER, ACCESSORY, LAUNCHER RECEPTACLE FOR MIL-STD-1760 APPLICATIONS (METRIC) |
DEFSTAN 00-970(PT9)/5(2009) : 2009 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 9: UAV SYSTEMS |
DEFSTAN 07-85(PT1)/3(2006) : 2006 | DESIGN REQUIREMENTS FOR WEAPONS AND ASSOCIATED SYSTEMS - PART 1: MANDATORY DESIGN REQUIREMENTS |
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-A-8591 Revision H:1990 | AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE); GENERAL DESIGN CRITERIA FOR |
SAE AS 4764 : 2017 | VALIDATION METHODS FOR MIL-STD-1760 AIRCRAFT STATION INTERFACES |
MIL-STD-2131 Revision A:1991 | LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR |
DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
SAE AS 5609 : 2017 | AIRCRAFT/STORE COMMON INTERFACE CONTROL DOCUMENT FORMAT STANDARD |
STANAG 3576 : 2016 | ELECTRICAL CONNECTOR FOR DISPENSERS AND INTERNAL INTERVALOMETER TYPE ROCKET LAUNCHERS FOR AIRCRAFT |
SAE AS 5653 : 2014 | HIGH SPEED NETWORK FOR MIL-STD-1760 |
DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
SAE AIR 4013 : 2012 | MULTIPLEX DATA BUS NETWORKS FOR MIL-STD-1760 STORES |
DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
MIL-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
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 |
MIL C 85629 : A (1) | CONTROL MONITOR SET GUIDED WEAPON, AN/AWW-13 |
MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
SAE AS 47641 : 2017 | VALIDATION METHODS FOR MIL-STD-1760B AIRCRAFT STATION INTERFACES |
JSSG-2001 Revision B:2004 | Air Vehicle |
SAE AS 5716 : 2012 | STANDARD ELECTRICAL AND LOGICAL INTERFACE FOR AIRBORNE FUZING SYSTEMS |
SAE AS 5725 : 2015 | INTERFACE STANDARD, MINIATURE MISSION STORE INTERFACE |
SAE AIR 6027 : 2017 | CONSIDERATIONS FOR SAFE STORE OPERATION ON MANNED AND UNMANNED VEHICLES |
SAE AS 42701 : 2014 | VALIDATION METHODS FOR MIL-STD-1760D MISSION STORES |
SAE AIR 6234 : 2016 | HANDBOOK: STANDARD ELECTRICAL AND LOGICAL INTERFACE FOR AIRBORNE FUZING SYSTEMS |
SAE AS 5726 : 2013 | INTERFACE STANDARD, INTERFACE FOR MICRO MUNITIONS |
MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
SAE AS 6089 : 2017 | VERIFICATION METHODS FOR AS5653 NETWORK CONTROLLER |
DEFSTAN 00-970(PT1)SEC6/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
MIL-STD-1289 Revision D:2003 | AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS |
SAE AS 47643 : 2017 | VERIFICATION METHODS FOR MIL-STD-1760E AIRCRAFT STATION INTERFACES |
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
SAE AS 4270 : 2017 | VALIDATION METHODS FOR MIL-STD-1760 MISSION STORES |
SAE AS 47642 : 2017 | VALIDATION METHODS FOR MIL-STD-1760C AIRCRAFT STATION INTERFACES |
SAE AIR 5683 : 2016 | HIGH PERFORMANCE 1553 RESEARCH AND DEVELOPMENT |
MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
MIL-DTL-83538-10 Revision B:2008 | CONNECTORS AND ACCESSORIES, ELECTRICAL, CIRCULAR, UMBILICAL, BUSHING, CABLE, LAUNCHER RECEPTACLE FOR MIL-STD-1760 APPLICATIONS (METRIC) |
MIL-DTL-83538-13 Revision A:2008 | CONNECTORS AND ACCESSORIES, ELECTRICAL, CIRCULAR, UMBILICAL, TEST PLUG, REMOVABLE CRIMP CONTACTS, PINS, FOR MIL-STD-1760 APPLICATIONS (METRIC) |
SAE ARD 50020 : A2003 | FIBER-OPTIC INTERCONNECTION HARDWARE FOR AEROSPACE APPLICATIONS |
AEP-100 : 2016 | ELECTRICAL CONNECTOR FOR DISPENSERS AND INTERNAL INTERVALOMETER TYPE ROCKET LAUNCHERS FOR AIRCRAFT |
MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
STANAG 3837 : 0 | AIRCRAFT STORES ELECTRICAL INTERCONNECTION SYSTEM |
SAE AS 39029/58 : 2015 | CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE (FOR MIL-DTL-24308, MIL-DTL-38999 SERIES 1, 2, 3, AND 4, AND MIL-DTL-55302/69 AND MIL-DTL-83733 CONNECTORS) |
SAE AS 5653 : 2014 | HIGH SPEED NETWORK FOR MIL-STD-1760 |
SAE AS 39029/114 : 2016 | CONTACT, ELECTRICAL CONNECTOR, CONCENTRIC TWINAX, SOCKET, SIZE 8, MIL-DTL-38999 SERIES 1, 3, AND 4 |
MIL-DTL-83538 Revision D:2006 | CONNECTORS AND ACCESSORIES, ELECTRICAL, CIRCULAR, UMBILICAL, ENVIRONMENT RESISTANT, REMOVABLE CRIMP CONTACTS FOR MIL-STD-1760 APPLICATIONS (METRIC), GENERAL SPECIFICATION FOR |
MIL-STD-8591 Base Document:2005 | AIRBORNE STORES, SUSPENSION EQUIPMENT AND AIRCRAFT-STORE INTERFACE (CARRIAGE PHASE) |
MIL-HDBK-1553 Revision A:1988 | Multiplex Application Handbook |
STANAG 3838 : 2016 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
SAE AS 85049 : 2016 | CONNECTOR ACCESSORIES, ELECTRICAL GENERAL SPECIFICATION FOR |
SAE AS 39029/56 : 2011 | CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR MIL-C-38999 SERIES 1, 3 AND 4 CONNECTORS) |
MIL C 17/113 : C | CABLE RADIO FREQUENCY FLEXIBLE COAXIAL 50 OHMS M 17/113 RG 316 |
MIL-DTL-38999 Revision M:2015 | Connectors, Electrical, Circular, Miniature, High Density, Quick Disconnect (Bayonet, Threaded or Breech Coupling), Environment Resistant with Crimp Removable Contacts or Hermetically Sealed with Fixed, Solderable Contacts, General Specification for |
STANAG 4294(PT1) : 1997 | NAVSTAR GLOBAL POSITIONING SYSTEM GPS PART 1-SYSTEM CHARACTERISTICS |
SAE AS 39029/75 : 2016 | CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, SHIELDED, SIZE 12 (FOR MIL-DTL-38999 SERIES 1, 3, AND 4 CONNECTORS) |
SAE AS 39029/113 : 2016 | CONTACT, ELECTRICAL CONNECTOR, CONCENTRIC TWINAX, PIN, SIZE 8, (FOR MIL-DTL- 38999 SERIES 1, 3, AND 4 CONNECTORS) |
MIL-STD-1560 Revision C:2015 | INSERT ARRANGEMENTS FOR MIL-DTL-38999, MIL-DTL-27599 AND SAE-AS29600 SERIES A - ELECTRICAL CIRCULAR CONNECTORS |
SAE AS 39029/28 : 2016 | CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, SHIELDED, SIZE 12 (FOR MIL-DTL-38999 SERIES 1, 2, 3 AND 4 CONNECTORS) |
SAE AS 39029 : 2017 | CONTACTS, ELECTRICAL CONNECTOR, GENERAL SPECIFICATION FOR |
SAE AS 39029/103 : 2016 | CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 12 (FOR MIL-DTL-38999 SERIES 1, 3 AND 4 CONNECTORS) |
SAE AS 39029/102 : 2016 | CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, COAXIAL, SIZE 12 (FOR MIL-DTL-38999 SERIES 1, 2, 3 AND 4 CONNECTORS) |
MS27488 Revision N:2008 | PLUG, END SEAL, ELECTRICAL CONNECTOR |
STANAG 3350 : 0 | ANALOGUE VIDEO STANDARD FOR AIRCRAFT SYSTEM APPLICATIONS |
MIL-STD-1553 Revision B:1978 | DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA |
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