• Shopping Cart
    There are no items in your cart

SAE ARD 50020 : A2003

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

FIBER-OPTIC INTERCONNECTION HARDWARE FOR AEROSPACE APPLICATIONS

Withdrawn date

25-06-2003

Published date

12-01-2013

Sorry this product is not available in your region.

1 Scope
2 Applicable documents
  2.1 Definitions
  2.2 Acronyms
  2.3 Metrication
3 Interconnect/harness problem areas
  3.1 Introductory statement
      3.1.1 Forum report
      3.1.2 Summary and Recommendations
  3.2 Overview of Harness Problems
      3.2.1 Electrical Wiring Concerns
      3.2.2 Fiber-Optic Concerns
      3.2.3 Interconnection Goals
      3.2.4 Avionics Trends
  3.3 Fiber-Optic Harness Concepts
      3.3.1 General Requirements
      3.3.2 Harness Structure
      3.3.3 Fiber
      3.3.4 Cable
      3.3.5 Conduit
      3.3.6 Connectors
      3.3.7 Backshell
      3.3.8 Termini
      3.3.9 Connector Mating adapter
      3.3.10 Splices
      3.3.11 Splitter/combiner
      3.3.12 Installation
  3.4 Power Budget Considerations
  3.5 Reflected Energy
  3.6 Supportability
      3.6.1 Maintainability
  3.7 Desired Interconnection Parameters
      3.7.1 Fiber, Glass, 850 nm Window
      3.7.2 Fiber, Glass, Long-Wave Window
      3.7.3 Fiber, Polymeric
      3.7.4 Cable
      3.7.5 Connector/Termination
4 RECOMMENDATIONS
5 KEY WORDS
APPENDIX A REFERENCES SOURCES OF INFORMATION
LIST OF FIGURES

Includes all aspects of the fiber-optic interconnection system needed for diverse applications within the aerospace industry.

Committee
AS-3
DocumentType
Standard
PublisherName
SAE International
Status
Withdrawn

SAE AIR 4922A : 2015 PRIMARY FLIGHT CONTROL HYDRAULIC ACTUATION SYSTEM INTERFACE DEFINITION
SAE ARD 50024 : A2003 FIBER OPTIC COUPLED SENSORS FOR AEROSPACE APPLICATIONS
SAE AIR 4982 : 2014 AEROSPACE FLY-BY-LIGHT ACTUATION SYSTEMS

ARINC 629 : 90 SUPP 5 MULTI TRANSMITTER DATA BUS - TECHNICAL DESCRIPTION
MIL-STD-1760 Revision E:2007 AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
ARINC 659 : 1993 BACKPLANE DATA BUS
MIL E 5400 : T ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR
MIL C 83723 : E CONNECTORS, ELECTRICAL (CIRCULAR, ENVIRONMENT RESISTING) RECEPTACLES AND PLUGS GENERAL SPECIFICATION FOR
MIL C 38999 : J CONNECTOR, ELECTRICAL, CIRCULAR, MINIATURE, HIGH DENSITY, QUICK DISCONNECT (BAYONET THREADED & BREECH COUPLING) ENVIRONMENT RESISTANT, REMOVABLE CRIMP & HERMETIC SOLDER CONTACTS
MIL-STD-1773 Base Document:1988 FIBER OPTICS MECHANIZATION OF AN AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS
MIL STD 1678 : NOTICE 1 FIBER OPTICS TEST METHODS AND INSTRUMENTATION
ARINC 404A : 1974 AIR TRANSPORT EQUIPMENT CASES AND RACKING

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.