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  • IEC TS 62396-5:2008

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    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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    Process management for avionics - Atmospheric radiation effects - Part 5: Guidelines for assessing thermal neutron fluxes and effects in avionics systems

    Available format(s):  Hardcopy, PDF, PDF 3 Users, PDF 5 Users, PDF 9 Users

    Superseded date:  22-08-2014

    Language(s):  English

    Published date:  19-08-2008

    Publisher:  International Electrotechnical Committee

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    Table of Contents - (Show below) - (Hide below)

    FOREWORD
    1 Scope
    2 Normative references
    3 Terms and definitions
    4 Overview of thermal neutron single event rate calculation
    5 Thermal neutron flux inside an airliner
      5.1 Definition of thermal neutron
      5.2 Overview
      5.3 Background on aircraft measurements
      5.4 Calculational approach
      5.5 Processing of in-flight neutron flux data
    6 Thermal neutron SEU cross sections
      6.1 Overview of the issue
      6.2 Mechanism involved
      6.3 Thermal neutron SEU cross sections and Ratio-2
    7 Recommendation for devices in avionics at present time
    Bibliography

    Abstract - (Show below) - (Hide below)

    IEC TS 62396-5:2008 (E) provides a more precise definition of the threat that thermal neutrons pose to avionics as a second mechanism for inducing single event upset (SEU) in microelectronics. Addresses more in detail the following: detailed evaluation of the existing literature on measurements of the thermal flux inside of airliners; an enhanced compilation of the thermal neutron SEU cross section in currently available SRAM devices (more than 20 different devices).

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    Development Note Supersedes IEC PAS 62396-5. (08/2008) Stability Date: 2013. (10/2012)
    Document Type Technical Specification
    Publisher International Electrotechnical Committee
    Status Superseded
    Superseded By
    Supersedes

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

    15/30324422 DC : 0 BS EN 62396-1 - PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 1: ACCOMMODATION OF ATMOSPHERIC RADIATION EFFECTS VIA SINGLE EVENT EFFECTS WITHIN AVIONICS ELECTRONIC EQUIPMENT
    BS IEC 62396-1 : 2016 PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 1: ACCOMMODATION OF ATMOSPHERIC RADIATION EFFECTS VIA SINGLE EVENT EFFECTS WITHIN AVIONICS ELECTRONIC EQUIPMENT
    11/30256756 DC : 0 BS EN 62396-2 - PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 2: GUIDELINES FOR SINGLE EVENT EFFECTS TESTING FOR AVIONICS SYSTEMS
    14/30299002 DC : 0 BS EN 60749-44 - SEMICONDUCTOR DEVICES - MECHANICAL AND CLIMATIC TEST METHODS - PART 44: NEUTRON BEAM IRRADIATED SINGLE EVENT EFFECT (SEE) TEST METHOD FOR SEMICONDUCTOR DEVICES
    11/30246255 DC : 0 BS EN 62396-1 - PROCESS MANAGEMENT FOR AVIONICS - ATMOSPHERIC RADIATION EFFECTS - PART 1: ACCOMMODATION OF ATMOSPHERIC RADIATION EFFECTS VIA SINGLE EVENT EFFECTS WITHIN AVIONICS ELECTRONIC EQUIPMENT
    PD IEC/PAS 62396-6:2014 Process management for avionics. Atmospheric radiation effects Extreme space weather and potential impact on the avionics environment and electronics

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

    IEC TS 62396-1:2006 Process management for avionics - Atmospheric radiation effects - Part 1: Accommodation of atmospheric radiation effects via single event effects within avionics electronic equipment
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