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DD IEC TS 62396-1 : DRAFT JUL 2006

Withdrawn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A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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Withdrawn date

27-10-2018

Published date

23-11-2012

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

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

Committee
GEL/107
DocumentType
Draft
PublisherName
British Standards Institution
Status
Withdrawn
SupersededBy

Standards Relationship
IEC TS 62396-1:2006 Identical

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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