MIL-STD-464 Revision C:2010
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
ELECTROMAGNETIC ENVIRONMENTAL EFFECTS REQUIREMENTS FOR SYSTEMS
Available format(s)
PDF
Superseded date
12-12-2022
Superseded by
Language(s)
English
Publisher
Important note : All end users must be registered with an Account prior to user licenses being assigned.
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
|
| DocumentType |
Standard
|
| Pages |
165
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| 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 AS 6129 : 2012 | 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 ARP 5120 : 2016 | 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 ARP 94910 : 2012 | 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 ARP 4945 : 2013 | 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 AS 19692 : 2016 | Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
| MIL PRF 0032381 : A | ACOUSTIC HAILING DEVICE (LIGHT) |
| SAE ARP 4404 : 2013 : R2019 | AIRCRAFT ELECTRICAL INSTALLATIONS |
| SAE AS 1650 : 2017 | 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 ARP 5770 : 2012 | 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 AS 50881 : 2015 | WIRING AEROSPACE VEHICLE |
| SAE AS 5652 : 2018 | 10 MEGABIT/SEC NETWORK CONFIGURATION DIGITAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS |
| AECTP-250 : 2014 | ELECTRICAL AND ELECTROMAGNETIC ENVIRONMENTAL CONDITIONS |
| SAE AS 94900 : 2007 | 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 ARP 5794 : 2014 | 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 AS 4941 : 2015 | AEROSPACE - GENERAL REQUIREMENTS FOR COMMERCIAL AIRCRAFT HYDRAULIC COMPONENTS |
| ANEP-45 : 0 | |
| SAE AS 5356 : 2017 | COUPLING, FUEL LINE, FLEXIBLE, 125 PSI GENERAL SPECIFICATION FOR |
| SAE ARP 5415 : 2008 | 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 AIR 825/12 : 2013 | 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:1987(S2012) | Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)<br> |
| 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 ARP 4242 : 1999(S2013) | 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 ARP 5416 : 2013 | 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 ARP 5414 : 2012 | 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 ARP 5412 : 2013 | 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 |
Access your standards online with a subscription
Features
-
Simple online access to standards, technical information and regulations.
-
Critical updates of standards and customisable alerts and notifications.
-
Multi-user online standards collection: secure, flexible and cost effective.