SAE AIR5271
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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
Hardcopy , PDF
22-07-2022
English
03-03-2009
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Superseded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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