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Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
English
01-12-2010
12-12-2022
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.
| 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Superseded
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| Supersedes |
This standard establishes electromagnetic environmental effects (E3) interface requirements and verification criteria for airborne, sea, space, and ground systems, including associated ordnance.
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| A-A-52316 Revision C:2010 | Tester, Construction Materials, Moisture & Density (TCMMD) |
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| 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 |
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| MIL-DTL-53078 Revision A:2011 | Mounting Kit: M1 Tank, Cleared Lane Marking System (Clams) |
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| 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) |
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| 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 |
| 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 |
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| 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 |
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| AEP-41 VOL 6 : 2014 | NATO IMPLEMENTATION OF UNIFIED PROTECTION AGAINST ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (UE[3]) |
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| ANEP-45 : 0 | |
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| MIL-DTL-23659 Revision F:2010 | Initiators, Electric, General Design Specification for |
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| ANEP-45 : 0 | |
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| 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 |
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| SAE ARP5416A | Aircraft Lightning Test Methods |
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| 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, (Handbook Contains both Volume I Basic Theory, and Volume II Applications) |
| MIL-HDBK-235-7 Base Document:2010 | Military Operational EME Profiles Part 7E External Electromagnetic Environment Levelsfor Ordnance |
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