• 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    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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

    Available format(s):  PDF

    Withdrawn date:  08-07-1996

    Language(s): 

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Abstract - (Show below) - (Hide below)

    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.

    General Product Information - (Show below) - (Hide below)

    Committee AREA EMCS
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Withdrawn

    Standards Referenced By This Book - (Show below) - (Hide below)

    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

    Standards Referencing This Book - (Show below) - (Hide below)

    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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