MIL-STD-1757 Revision A:1983
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
LIGHTNING QUALIFICATION TEST TECHNIQUES FOR AEROSPACE VEHICLES AND HARDWARE
08-07-1996
Important note : Users cannot be edited or removed once added to your Multi user PDF.Defines standard test waveforms and procedures for lightning qualification testing of aerospace vehicles and hardware. Coverage includes reference documents, definitions, equipment calibration, voltage waveforms, hot spot testing, test electrodes, photographic techniques, fast flux (aperture) coupling, and restive/diffusion flux induced voltages. Also gives detailed diagrams.
| Committee |
AREA EMCS
|
| DocumentType |
Standard
|
| Pages |
99
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL D 9129 : D | DISCHARGERS, ELECTROSTATIC - GENERAL SPECIFICATION FOR |
| RE.AERO 70251 : A1993 | AIRCRAFT PROTECTION AGAINST THE EFFECTS OF LIGHTNING - AFFECTIVITY TESTS |
| JSSG-2010-5 Base Document:1998 | Crew Systems Aircraft Lighting Handbook |
| 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)/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)/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)/8(2011) : 2011 | 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-STD-1541 Revision A:1987 | ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR SPACE SYSTEMS |
| MIL-HDBK-87244 Base Document:1995 | AVIONICS/ELECTRONICS INTEGRITY |
| AFGS-87266 Base Document:1992 | AIRCRAFT COCKPIT TRANSPARENCY SYSTEM |
| SAE AIR 5128 : 2012 | ELECTRICAL BONDING OF AIRCRAFT FUEL SYSTEMS |
| JSSG-2006 Base Document:1998 | JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES |
| AOP 25 : 1999 | RATIONALE AND GUIDANCE CONCERNING STANAG 4327, LIGHTNING, MUNITION ASSESSMENT AND TEST PROCEDURES |
| MIL-I-8671 Revision D:1994 | INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS |
| MIL-D-8708 Revision C:1991 | DEMONSTRATION REQUIREMENTS FOR AIRPLANES |
| EIA IS 647 : 1996 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE EMISSIONS AND SUSCEPTIBILITY CHARACTERISTICS OF EQUIPMENT INTENDED TO OPERATE IN SEVERE ELECTROMAGNETIC ENVIRONMENTS |
| MIL-STD-45662 Revision A:1988 | CALIBRATION SYSTEMS REQUIREMENTS |
| IEEE 4-2013 | IEEE Standard for High-Voltage Testing Techniques |
| MIL C 45662 : 0 | CALIBRATION SYSTEM REQUIREMENTS |
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