• DD IEC TS 62396-1 : DRAFT JUL 2006

    Withdrawn A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

    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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    Withdrawn date:  27-10-2018

    Language(s): 

    Published date:  23-11-2012

    Publisher:  British Standards Institution

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

    FOREWORD
    INTRODUCTION
    1 Scope and object
    2 Normative references
    3 Terms and definitions
    4 Abbreviations used in the document
    5 Radiation environment of the atmosphere
      5.1 Radiation generation
      5.2 Effect of secondary particles on avionics
      5.3 Atmospheric neutrons
      5.4 Secondary protons
      5.5 Other particles
      5.6 Solar enhancements
    6 Effects of atmospheric radiation on avionics
      6.1 Types of radiation effects
      6.2 Single event effects
      6.3 Total Ionising Dose (TID)
      6.4 Displacement damage
    7 Guidance for system designs
      7.1 Overview
      7.2 System design
      7.3 Hardware considerations
      7.4 Parts characterisation and control
    8 Determination of avionics single event effects rates
      8.1 Main single event effects
      8.2 Single event effects with lower event rates
      8.3 Single event effects with higher event rates -
          Single event upset data
      8.4 Calculating SEE rates in avionics
    9 Considerations for SEE compliance
      9.1 Compliance
      9.2 Confirm the radiation environment for the
          avionics application
      9.3 Identify system development assurance level
      9.4 Assess preliminary electronic equipment design
          for SEE
      9.5 Verify that the system development assurance level
          requirements are met for SEE
      9.6 Corrective actions
    Annex A (informative) Thermal neutron assessment
    Annex B (informative) Methods of calculating SEE rates
            in avionics electronics
    Annex C (informative) Review of test facility availability
    Annex D (informative) Tabular description of variation of
            atmospheric neutron flux with altitude and
            latitude

    Abstract - (Show below) - (Hide below)

    Specifies the radiation environment, the effects of that environment on electronics and provides design considerations for the accommodation of those effects within avionics systems.

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

    Comment Closes On
    Committee GEL/107
    Document Type Draft
    Publisher British Standards Institution
    Status Withdrawn
    Superseded By

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

    MIL-STD-883 Revision K:2016 TEST METHOD STANDARD - MICROCIRCUITS
    SAE ARP 4754 : 2010 GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
    MIL-PRF-19500 Revision P:2010 SEMICONDUCTOR DEVICES, GENERAL SPECIFICATION FOR
    SAE ARP 4761 : 1996 GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
    FAA AC 23.1309-1 : 2011 SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES
    FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
    MIL-PRF-38535 Revision K:2013 Integrated Circuits (Microcircuits) Manufacturing, General Specification for
    AIAA R 100 : A 2001 RECOMMENDED PRACTICE FOR PARTS MANAGEMENT
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