MIL-STD-464 Revision C:2010
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
12-12-2022
English
FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS
4. GENERAL REQUIREMENTS
5. DETAILED REQUIREMENTS
6. NOTES
APPENDIX A - APPLICATION GUIDE
Describes electromagnetic environmental effects (E3) interface requirements and verification criteria for airborne, sea, space, and ground systems, including associated ordnance.
Committee |
AREA EMCS
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DocumentType |
Standard
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Pages |
165
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PublisherName |
US Military Specs/Standards/Handbooks
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Status |
Superseded
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SupersededBy | |
Supersedes |
SAE AIR 4004 : 2015 | GUIDE FOR INSTALLATION OF ELECTRICAL WIRE AND CABLE ON AIRCRAFT LANDING GEAR |
16/30337938 DC : 0 | BS EN 80005-1 - UTILITY CONNECTIONS IN PORT - HIGH VOLTAGE SHORE CONNECTION (HVSC) SYSTEMS - PART 1: GENERAL REQUIREMENTS |
SAE AS6129 | AS6129: Interface Standard, Airborne EO/IR Systems, Electrical |
MIL-PRF-32316 Base Document:2008 | RIFLE, 7.62 MM: SEMI-AUTOMATIC SNIPER SYSTEM (SASS) - M110 |
MIL-PRF-71185 Revision A:2013 | Dynamic Reference Unit-Hybrid-Replacement (DRU-H-R) |
MIL-STD-1901 Revision A:2002 | MUNITION ROCKET AND MISSILE MOTOR IGNITION SYSTEM DESIGN, SAFETY CRITERIA FOR |
13/30286075 DC : 0 | BS EN 61000-4-36 ED 1.0 - ELECTROMAGNETIC COMPATIBILITY (EMC) - PART 4-36: TESTING AND MEASUREMENT TECHNIQUES - IEMI IMMUNITY TEST METHODS FOR EQUIPMENT AND SYSTEMS |
MIL-DTL-32151 Revision A:2006 | IMPULSE CARTRIDGE, CCU-71/A |
MIL-STD-1791 Revision C:2017 | DESIGNING FOR INTERNAL AERIAL DELIVERY IN FIXED WING AIRCRAFT |
MIL-PRF-83419 Revision F:2016 | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
STANREC 4567 : 2014 | NATO IMPLEMENTATION OF UNIFIED PROTECTION AGAINST ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE3) |
SAE ARP5120 | Aircraft Gas Turbine Engine Health Management System Development and Integration Guide |
NFPA 780 : 2017 | INSTALLATION OF LIGHTNING PROTECTION SYSTEMS |
DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-STD-2088 Revision B:2007 | BOMB RACK UNIT (BRU), SINGLE STORE, AIRCRAFT |
DEFSTAN 00-970(PT0)/17(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
AIAA G-082:2022 | Guide: Space Systems — Composite Overwrapped Pressure Vessels with a Plastic Liner |
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 |
MIL-PRF-32565 Revision A:2017 | BATTERY, RECHARGEABLE, SEALED, 6T LITHIUM-ION |
MIL-DTL-32106 Base Document:2003 | INITIATORS, ELECTRICAL, FOR ROCKET MOTOR IGNITERS |
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)/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)/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-PRF-7115 Revision G:2012 | CONVERTERS, AIRCRAFT, GENERAL SPECIFICATION FOR |
DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-DTL-27723 Revision F:2013 | Probe, Total Temperature, Deiceable |
DEFSTAN 00-970(PT0)/16(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
ANEP-80 : 2009 | NATO SONOBUOY INTEROPERABILITY SPECIFICATION - COMMON SPECIFICATIONS |
DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
MIL-HDBK-240 Revision A:2011 | HAZARDS OF ELECTROMAGNETIC RADIATION TO ORDNANCE TEST GUIDE |
DI-MGMT-81826 Revision C:2014 | F/A-18 and EA-18 Aircraft / System Program Protection Implementation Plan |
MIL-DTL-15370 Revision K:2015 | COUPLERS, DIRECTIONAL, GENERAL SPECIFICATION FOR |
SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
AFGS-87219 Revision B:2012 | ELECTRICAL POWER SYSTEMS, AIRCRAFT |
MIL-PRF-53024 Revision C:2012 | COMPACTOR, HIGH SPEED, SELF-PROPELLED, COMMERCIAL CONSTRUCTION EQUIPMENT (CCE) |
MIL-HDBK-510 Revision A:2014 | AEROSPACE FUELS CERTIFICATION |
NASA MSFC STD 1800 : 2008 | ELECTROSTATIC DISCHARGE (ESD) CONTROL FOR PROPELLANT AND EXPLOSIVE DEVICES |
A-A-52316 Revision C:2010 | TESTER, CONSTRUCTION MATERIALS, MOISTURE & DENSITY (TCMMD) |
NASA STD 7002 : 0 | PAYLOAD TEST REQUIREMENTS |
MIL-DTL-32572 Base Document:2017 | Anchor Windlass, Electro-Mechanical, Vertical, Two-Speedand Variable-Speed |
MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
SAE ARP94910 | Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For |
SAE AS 6169A : 2013 | INTERFACE STANDARD, AIRBORNE EO/IR SYSTEMS, MECHANICAL |
SAE ARP4945A | Aerospace-Solenoid Valve, Hydraulic, Three Way, Two Position, Direct Acting |
IEC 61000-4-36:2014 | Electromagnetic compatibility (EMC) - Part 4-36: Testing and measurement techniques - IEMI immunity test methods for equipment and systems |
MIL-DTL-32015 Base Document:1999 | MICROPHONES, LINEAR, GENERAL SPECIFICATION FOR |
MIL-HDBK-516 Revision C:2014 | AIRWORTHINESS CERTIFICATION CRITERIA |
AEP-62 VOL 7 : 2013 | PROCEDURES FOR TESTING AND EVALUATION PERFORMANCE LEVELS OF DAS (DEFENSIVE AIDS SUITES) FOR ARMOURED VEHICLES - VOLUME 7: PROCEDURE FOR THE ASSESSMENT OF INTEGRATION |
MIL-STD-1310 Revision H:2009 | SHIPBOARD BONDING, GROUNDING, AND OTHER TECHNIQUES FOR ELECTROMAGNETIC COMPATIBILITY, ELECTROMAGNETIC PULSE (EMP) MITIGATION, AND SAFETY |
MIL-HDBK-510-1 Revision A:2010 | AEROSPACE FUELS CERTIFICATION |
SAE ARP 5311 : 2016 | AEROSPACE-INTERFACE DEFINITION FOR MECHANICAL ACTUATION SUBSYSTEMS |
MIL-DTL-32188 Base Document:2005 | INITIATOR, MECHANICAL ACTUATED JAU-25/A |
MIL-HDBK-1760 Revision A:2004 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
MIL-STD-331 Revision D:2017 | FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR |
MIL-PRF-32381 Revision B:2016 | Acoustic Hailing Device (Light) |
MIL-STD-1605 Revision A:2009 | Procedures for Conducting a Shipboard Electromagnetic Interference (EMI) Survey (Surface Ship) |
SAE AIR 5128 : 2012 | ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEMS |
NASA KSC STD E 0022 : 2013 | BONDING, GROUNDING, SHIELDING, ELECTROMAGNETIC INTERFERENCE, LIGHTNING AND TRANSIENT PROTECTION, DESIGN REQUIREMENTS FOR GROUND SYSTEMS |
MIL-HDBK-1763 Base Document:1998 | AIRCRAFT/STORES COMPATIBILITY: SYSTEMS ENGINEERING DATA REQUIREMENTS AND TEST PROCEDURES |
MIL-PRF-53051 Revision C:2017 | PUMPING ASSEMBLIES, WHEEL-MOUNTED, DIESEL ENGINE DRIVEN, BULK TRANSFER, FUEL AND POTABLE WATER PUMPING SERVICE |
JSSG-2001 Revision B:2004 | Air Vehicle |
MIL-DTL-32193 Base Document:2005 | INITIATOR, EXPLOSIVE ACTUATED, JAU-29/A |
MIL-HDBK-274 Revision A:2011 | ELECTRICAL GROUNDING FOR AIRCRAFT SAFETY |
MIL-PRF-32516 Base Document:2015 | ELECTRONIC TEST EQUIPMENT, INTERMITTENT FAULT DETECTION AND ISOLATION FOR CHASSIS AND BACKPLANE CONDUCTIVE PATHS |
SAE AS19692B | Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
MIL PRF 0032381 : A | ACOUSTIC HAILING DEVICE (LIGHT) |
SAE ARP4404C | Aircraft Electrical Installations |
SAE AS1650E | Coupling Assembly, Threadless, Flexible, Fixed Cavity, Self-Bonding, Procurement Specification |
IEEE 1709-2010 | IEEE Recommended Practice for 1 kV to 35 kV Medium-Voltage DC Power Systems on Ships |
NASA KSC E 165 : 2009 | ELECTRICAL GROUND SUPPORT EQUIPMENT FABRICATION, SPECIFICATION FOR |
NASA MSFC SPEC 3635 : 2012 | PYROTECHNIC SYSTEM SPECIFICATION |
MIL-DTL-53078 Revision A:2011 | MOUNTING KIT: M1 TANK CLEARED LANE MARKING SYSTEM (CLAMS) |
NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
NASA KSC STD E 0001 : 2008 | DESIGN OF ELECTRICAL CONTROL AND MONITORING SYSTEMS, EQUIPMENT (GSE), AND PANELS, STANDARD FOR |
NASA STD 8719.24 : 2011 | NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
NASA MSFC HDBK 3697 : 2014 | ELECTRICAL BONDING DESIGN GUIDE HANDBOOK |
MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
MIL-DTL-83361 Revision B:2007 | INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A |
MIL-PRF-57267 Base Document:2017 | COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5 |
IPC HDBK 630 : 0 | GUIDELINES FOR DESIGN, MANUFACTURE, INSPECTION AND TESTING OF ELECTRONIC ENCLOSURES ASSEMBLY |
SAE ARP5770 | Mechanical Control Design Guide |
BS ISO/IEC/IEEE 80005-1:2012 | Utility connections in port High Voltage Shore Connection (HVSC) Systems. General requirements |
MIL-DTL-9490 Revision E:2008 | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
MIL-DTL-85097-13 Revision C:2000 | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET MOTOR, CANOPY JETTISON, MARK 109 MODS 0 AND 1 (LOADED ASSEMBLIES) |
NASA MSFC SPEC 521 : 2013 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR EQUIPMENT AND SUBSYSTEMS |
MIL-DTL-82960 Revision B:2010 | INITIATOR, PROPELLANT ACTUATED, JAU-27/A (MF72) |
NASA STD 4003 : 2013 | ELECTRICAL BONDING FOR NASA LAUNCH VEHICLES, SPACECRAFT, PAYLOADS, AND FLIGHT EQUIPMENT |
SAE ARP 5672 : 2016 | AIRCRAFT PRECIPITATION STATIC CERTIFICATION |
JSSG-2009 Revision A:2013 | Air Vehicle Subsystems |
MIL-STD-7179 Revision A:2009 | Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems and Support Equipment |
AEP-41 VOL 1 : 2004 | UNIFIED ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE[3]) PROTECTION, PHILOSOPHY AND METHODOLOGY |
MIL-PRF-83323 Revision D:2016 | TESTER, UNIVERSAL RECEPTACLE, AERIAL REFUELING |
ADS-63-SP : 2001 | AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS |
MIL-PRF-52955 Revision D:2009 | IMPROVED POSITION AND AZIMUTH DETERMINING SYSTEM (IPADS) |
MIL-STD-1316 Revision F:2017 | Fuze Design, Safety Criteria for |
MIL-DTL-32194 Revision B:2009 | IMPULSE CARTRIDGE, CCU-72/A |
MIL-STD-1289 Revision D:2003 | AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS |
JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
MIL-PRF-32293 Base Document:2008 | Cap, Blasting, Electric - M6 |
SAE ARP 4404 : 2013 | AIRCRAFT ELECTRICAL INSTALLATIONS |
SAE AS 6479 : 2014 | SPLICER, FUSION, FIBER OPTIC, AEROSPACE |
AEP-24 : 2006 | AIRCRAFT ELECTRICAL HAZARDS ON THE FLIGHT LINE |
SAE AS50881F | Wiring Aerospace Vehicle |
SAE AS5652A | 10 Megabit/sec Network Configuration Digital Time Division Command/Response Multiplex Data Bus |
AECTP-250 : 2014 | ELECTRICAL AND ELECTROMAGNETIC ENVIRONMENTAL CONDITIONS |
SAE AS94900 | Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For |
BS IEC 61000-4-36:2014 | Electromagnetic compatibility (EMC) Testing and measurement techniques. IEMI immunity test methods for equipment and systems |
MIL-HDBK-235-1 Revision C:2010 | MILITARY OPERATIONAL ELECTROMAGNETIC ENVIRONMENT PROFILES - PART 1: GENERAL GUIDANCE |
AEP-41 VOL 6 : 2014 | NATO IMPLEMENTATION OF UNIFIED PROTECTION AGAINST ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE[3]) |
MIL-PRF-32294 Base Document:2008 | Cap, Blasting, Non-Electric - M7 Cap, Blasting, Practice, Inert, Non-Electric - XM30 |
ADS-65-HDBK : 2004 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS |
AECTP-500 : 2016 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS TESTS AND VERIFICATION |
MIL-DTL-28875 Revision C:2012 | Amplifiers, Radio-Frequency and Microwave, Solid-State, General Specification for |
MIL-DTL-23659 Revision F:2010 | Initiators, Electric, General Design Specification for |
IEEE C62.55-2017 | IEEE Guide for Surge Protection of DC Power Feeds to Remote Radio Heads |
MIL-DTL-62421 Revision A:2009 | CONTROL, UNIT, ELECTRONIC, DIGITAL |
SAE AIR 5774 : 2012 | COMPOSITE FUEL TANKS, FUEL SYSTEM DESIGN CONSIDERATIONS |
SAE ARP5794 | Centrifugal Aircraft Fuel Pump Requirements, Design and Testing, Aerospace Standard |
MIL-HDBK-237 Revision D:2005 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS AND SPECTRUM SUPPORTABILITY GUIDANCE FOR THE ACQUISITION PROCESS |
SAE ARP 60493 : 2017 | GUIDE TO CIVIL AIRCRAFT ELECTROMAGNETIC COMPATIBILITY (EMC) |
AEP-41 VOL 7 : 2014 | NATO IMPLEMENTATION OF UNIFIED PROTECTION AGAINST ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE[3]) - VOLUME 7: SUSTAINMENT TEST AND EVALUATION |
AEP-41 VOL 2 : 2004 | ELECTROMAGNETIC (EM), ENVIRONMENTS (EMES), EM ENVIRONMENTAL EFFECTS (E[3]) AND OPERATIONAL CATEGORIES (OCS) |
SAE AS4941B | Aerospace - General Requirements for Commercial Aircraft Hydraulic Components |
ANEP-45 : 0 | |
SAE AS5356B | Coupling, Fuel Line, Flexible, 125 psi General Specification for |
SAE ARP5415A | User\'s Manual for Certification of Aircraft Electrical/Electronic Systems for the Indirect Effects of Lightning |
IEEE/ANSI C63.14-2014 REDLINE | American National Standard Dictionary of Electromagnetic Compatibility (EMC) including Electromagnetic Environmental Effects (E3) |
IEEE/ANSI C63.26-2015 | IEEE/ANSI Standard for Compliance Testing of Transmitters Used in Licensed Radio Services |
SAE AIR825/12A | Oxygen System Integration and Performance Precautions |
AAS3P-10 : 2011 | SAFETY AND SUITABILITY FOR SERVICE ASSESSMENT TESTING FOR SHOULDER LAUNCHED MUNITIONS |
IEC/ISO/IEEE 80005-1:2012 | Utility connections in port - Part 1: High Voltage Shore Connection (HVSC) Systems - General requirements |
MIL-STD-704 Revision F:2004 | AIRCRAFT ELECTRIC POWER CHARACTERISTICS |
ISO 46:1973 | Aircraft — Fuel nozzle grounding plugs and sockets |
FAA AC 20-53 : 2006 | PROTECTION OF AIRCRAFT FUEL SYSTEMS AGAINST FUEL VAPOR IGNITION CAUSED BY LIGHTNING |
MIL-STD-1541 Revision A:1987 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR SPACE SYSTEMS |
FAA AC 20-136 : 2011 | AIRCRAFT ELECTRICAL AND ELECTRONIC SYSTEM LIGHTNING PROTECTION |
NFPA 780 : 2017 | INSTALLATION OF LIGHTNING PROTECTION SYSTEMS |
MIL-STD-449 Revision D:1973 | MEASUREMENT OF RADIO FREQUENCY SPECTRUM CHARACTERISTICS |
MIL-HDBK-83578 Base Document:1999 | CRITERIA FOR EXPLOSIVE SYSTEMS AND DEVICES USED ON SPACE VEHICLES |
MIL-STD-1542 Revision B:1991 | |
MIL-STD-188-125-2 Base Document:1999 | HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR GROUND-BASED C[4]I FACILITIES PERFORMING CRITICAL, TIME-URGENT MISSIONS - PART 2 - TRANSPORTABLE SYSTEMS |
MIL-HDBK-235-10 Base Document:2010 | MILITARY OPERATIONAL ELECTROMAGNETIC ENVIRONMENT PROFILES - PART 10: EXTERNAL ELECTROMAGNETIC ENVIRONMENT LEVELS FOR SUBMARINE OPERATIONS |
MIL-HDBK-1568 Base Document:1996 | MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
AECTP-500 : 2016 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS TESTS AND VERIFICATION |
MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
SAE ARP 5415 : 2002 | USER'S MANUAL FOR CERTIFICATION OF AIRCRAFT ELECTRICAL/ELECTRONIC SYSTEMS FOR THE INDIRECT EFFECTS OF LIGHTNING |
MIL-STD-1605 Revision A:2009 | Procedures for Conducting a Shipboard Electromagnetic Interference (EMI) Survey (Surface Ship) |
MIL-STD-188-124 Revision B:1992 | GROUNDING BONDING AND SHIELDING FOR COMMON LONG HAUL TACTICAL COMMUNICATION SYSTEMS INCLUDING GROUND BASED COMMUNICATIONS ELECTRONICS FACILITIES & EQUIPMENTS |
MIL-DTL-23659 Revision F:2010 | Initiators, Electric, General Design Specification for |
MIL-STD-1310 Revision H:2009 | SHIPBOARD BONDING, GROUNDING, AND OTHER TECHNIQUES FOR ELECTROMAGNETIC COMPATIBILITY, ELECTROMAGNETIC PULSE (EMP) MITIGATION, AND SAFETY |
SAE ARP1870A | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety |
ANEP-45 : 0 | |
MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
MIL-HDBK-423 Base Document:1993 | HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR FIXED AND TRANSPORTABLE GROUND - BASED C4 1 FACILITIES - VOLUME 1 - FIXED FACILITIES |
SAE ARP4242A | Electromagnetic Compatibility Control Requirements Systems |
NFPA 70 : 2017 | NATIONAL ELECTRICAL CODE |
MIL-HDBK-235-1 Revision C:2010 | MILITARY OPERATIONAL ELECTROMAGNETIC ENVIRONMENT PROFILES - PART 1: GENERAL GUIDANCE |
MIL-STD-1399-300 Revision B:2008 | ELECTRIC POWER, ALTERNATING CURRENT |
MIL-STD-1576 Base Document:1984 | ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS |
DOD-STD-1399-70-1 Base Document:1979 | INTERFACE STANDARD FOR SHIPBOARD SYSTEMS SECTION 070 - PART 1: D.C. MAGNETIC FIELD ENVIRONMENT (METRIC) |
SAE ARP5416A | Aircraft Lightning Test Methods |
IEC 61000-2-9:1996 | Electromagnetic compatibility (EMC) - Part 2: Environment - Section 9: Description of HEMP environment - Radiated disturbance. Basic EMC publication |
SAE ARP 5577 : 2002 | AIRCRAFT LIGHTNING DIRECT EFFECTS CERTIFICATION |
SAE ARP5414A | Aircraft Lightning Zone |
MIL-HDBK-237 Revision D:2005 | ELECTROMAGNETIC ENVIRONMENTAL EFFECTS AND SPECTRUM SUPPORTABILITY GUIDANCE FOR THE ACQUISITION PROCESS |
MIL-HDBK-240 Revision A:2011 | HAZARDS OF ELECTROMAGNETIC RADIATION TO ORDNANCE TEST GUIDE |
MIL-STD-188-125-1 Base Document:1998 | HIGH-ALTITUDE ELECTROMAGNETIC PULSE (HEMP) PROTECTION FOR GROUND-BASED C[4]1 FACILITIES PERFORMING CRITICAL, TIME-URGENT MISSIONS PART 1 FIXED FACILITIES |
MIL-STD-331 Revision D:2017 | FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR |
SAE ARP5412B | Aircraft Lightning Environment and Related Test Waveforms |
MIL-HDBK-274 Revision A:2011 | ELECTRICAL GROUNDING FOR AIRCRAFT SAFETY |
MIL-DTL-83413 Revision C:2012 | CONNECTORS AND ASSEMBLIES, ELECTRICAL, AIRCRAFT GROUNDING, GENERAL SPECIFICATION FOR |
CFR 47(PTS80-END) : OCT 2017 | TELECOMMUNICATION - FEDERAL COMMUNICATIONS COMMISSION |
MIL-HDBK-83575 Base Document:1998 | GENERAL HANDBOOK FOR SPACE VEHICLE WIRING HARNESS DESIGN AND TESTING |
MIL-HDBK-419 Revision A:1987 | GROUNDING, BONDING, AND SHIELDING FOR ELECTRONIC EQUIPMENTS AND FACILITIES - VOLUME 1: BASIC THEORY & VOLUME 2: APPLICATIONS |
MIL-HDBK-235-7 Base Document:2010 | MILITARY OPERATIONAL ELECTROMAGNETIC ENVIRONMENT PROFILES - PART 7: EXTERNAL ELECTROMAGNETIC ENVIRONMENT LEVELS FOR ORDNANCE |
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