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SAE AIR5271

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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A Guideline for Application of High-Density Fiber Optic Interconnects to Aerospace Platforms

Available format(s)

Hardcopy , PDF

Superseded date

22-07-2022

Superseded by

SAE AIR5271A

Language(s)

English

Published date

03-03-2009

€178.75
Excluding VAT

1 Scope
2 Available reference documents
   2.1 Sources for reference documents
   2.2 Definitions
   2.3 First generation fibre optic interconnect
       constraints
   2.4 System requirements
   2.5 Fibre optic High-Density cable plant benefits
3 Advanced interconnect/harness requirements
4 Emerging technology trends
   4.1 Optical fibers for High-Density cables
   4.2 Optical fiber physical properties
   4.3 Optical properties of fibers
   4.4 Fiber optic ribbon cable construction
   4.5 High density fiber optic termination concepts
   4.6 Silicon compatible integrated optic devices
   4.7 Optical backplane interconnect
   4.8 Opto-Electronic source/detector devices and
       packaging
   4.9 Switching mechanisms
5 Optical amplifiers
   5.1 Erbium doped fiber amplifiers (EDFA)
   5.2 Semiconductor optical amplifiers (SOA)
   5.3 Comparison of SOA and EDFA performance
6 Aircraft installation
   6.1 Conduit enclosed cables
   6.2 Stand Alone Cable
   6.3 Air blown fiber (ABF)
   6.4 Splicing
   6.5 Branching and break-out techniques
   6.6 Fasteners or Tie-down techniques
   6.7 Installation and repair tools
7 Time division multiplexed network topologies
   7.1 Linear network topology
   7.2 Star network topology
   7.3 Ring network topology
   7.4 Mesh network topology
   7.5 Switched network topologies
   7.6 Shunted ring 'Skip-A-Node' topology
8 Broadband networks
   8.1 Sub-Carrier modulation
   8.2 Wavelength division multiplexing (WDM)
   8.3 Broadband Network topologies
9 Built-In-Test concepts
   9.1 Diagnostic requirements
   9.2 Functional element module
   9.3 Transmitter/Monitor and Receiver/Stimulator
10 Test equipment and maintenance
11 Advanced interconnect conclusions and recommendations
Appendix A - Reference sources
Appendix B - List of figures

Includes the basic attributes of a second-generation robust, reliable high-density fiber optic interconnect system for aerospace applications.

DocumentType
Standard
Pages
116
PublisherName
SAE International
Status
Superseded
SupersededBy
Supersedes

This SAE Aerospace Information Report (AIR5271) covers the basic attributes of a second-generation robust, reliable high-density fiber optic interconnect system for aerospace applications. The intent is to take advantage of recent commercial developments in materials, components and manufacturing methods to develop rugged high-density fiber optic interconnects optimized for aerospace and automotive applications, which can accommodate a variety of optical fiber waveguide types. These waveguide types include single mode and multi-mode glass/glass fibers and waveguides, plastic clad silica fibers and waveguides, and all polymer fibers and waveguides. This second generation interconnect system should represent a dramatic improvement over first generation. The cable should be extremely robust eliminating any concerns over cable damage or fiber breakage in an aerospace environment.A high-density fiber optic interconnect system provides the physical medium for optical data and control communication in aerospace vehicles. As such, it consists of the cables and harnesses, connectors, splices, backplane interfaces, transceivers, fiber optic couplers, and includes test and maintenance concepts for these items. Also included are manufacturing, installation and repair tools, processes and training programs. The high-density format should provide for both redundant serial data transmission or parallel data transfer by providing a scaleable fiber count. Connectors should provide an extremely small footprint, with low mass connector shells and array inserts, and accommodate both single and multi-mode fibers. Fiber spacing and cladding diameter should be standardized and coatings utilized to guarantee long term reliability. The cable connector interface shall be optimized to preclude damage during installation and/or maintenance actions as well as ease of termination. All elements of the cable plant should be compatible including splices and couplers with minimum weight, volume and footprint. This optimized cable plant shall serve as an integrated information distribution system capable of transferring all information on military and commercial aircraft with dramatic improvements in affordability, reliability, fault tolerance, EMI/EMP immunity and safety. Utilization of this cable plant will improve aircraft performance and fuel economy, providing operational cost effectiveness while reducing new aircraft certification costs.

MIL C 83522 : D CONNECTORS, FIBER OPTIC, SINGLE TERMINUS, GENERAL SPECIFICATION FOR
MIL-STD-883 Revision K:2016 TEST METHOD STANDARD - MICROCIRCUITS
ARINC 628-6 : 2002 CABIN EQUIPMENT INTERFACES - PART 6: FIBER OPTIC CABLE ASSEMBLY GENERAL SPECIFICATION
ARINC 636 : 1993 ON-BOARD LOCAL AREA NETWORK
ARINC 629-2 : 1996 SUPP 2 MULTI-TRANSMITTER DATA BUS - PART 2: APPLICATIONS GUIDE
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
AS 1773-1996 Articulated vehicles - Fifth wheel assemblies
MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
MIL-STD-1344 Revision A:1977 TEST METHODS FOR ELECTRICAL CONNECTORS
MIL STD 1678 : NOTICE 1 FIBER OPTICS TEST METHODS AND INSTRUMENTATION
MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
MIL-STD-202 Revision H:2015 ELECTRONIC AND ELECTRICAL COMPONENT PARTS
MIL F 49291 : B (1) FIBER, OPTICAL, (METRIC) GENERAL SPECIFICATION FOR USER: AV REVIEWER: 11 13 99 AR EC ES M1 OS SC
MIL C 85045 : E CABLES, FIBER OPTICS, (METRIC), GENERAL SPECIFICATION FOR
ARINC 404A : 1974 AIR TRANSPORT EQUIPMENT CASES AND RACKING
MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
GR 326 CORE : ISSUE 4 GENERIC REQUIREMENTS FOR SINGLE-MODE OPTICAL CONNECTORS AND JUMPER ASSEMBLIES

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