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IEC TS 62396-1:2006

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

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

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

08-03-2006

Withdrawn date

15-02-2019

Superseded by

IEC 62396-1:2016

€344.48
Excluding VAT
Summarise this standard

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

Provides guidance on atmospheric radiation effects on avionics electronics used in aircraft operating at altitudes up to 60 000 feet (18,3 km). Defines the radiation environment, the effects of that environment on electronics and provides design considerations for the accommodation of those effects within avionics systems. Is intended to help aerospace equipment manufacturers and designers to standardise their approach to single event effects in avionics.

Committee
TC 107
DocumentType
Technical Specification
Pages
58
PublisherName
International Electrotechnical Committee
Status
Withdrawn
SupersededBy

⚠

A newer version of this standard is available.

€344.48
Excluding VAT