1、AEROSPACE STANDARD CABLE, FIBER OPTIC, MULTI-MODE, 200/230/500 m, STEP INDEX, TIGHT BUFFER AS5382/6Copyright 2011 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, ph
2、otocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 2004-04REVISED 2011-10TH
3、IRD ANGLE PROJECTION CUSTODIAN: AE-8/AE-8D REV.AFEDERAL SUPPLY CLASS 6010 AS5382/6SHEET 1 OF 4REV. APROCUREMENT SPECIFICATION: NONESAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse ofthis report is entirely
4、 voluntary, andits applicability and suitability forany particular use,including any patent infringement arising therefrom, isthe soleresponsibilityofthe user.”SAE reviews eachtechnicalreport at least every five years at which time itmay bereaffirmed, revised, orcancelled. SAE invites yourwrittencom
5、ments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS5382/6ARATIONALE THIS DOCUMENT IS OVERDUE FOR ITS FIVE YEAR REVIEW AND REVIEW OF THE DOCUMENT NECESSITATES ELIMINATION OF ONE FLUID,1,1,1 TRICHLOROETHANE, FR
6、OM THE LIST OF IMMERSION TEST FLUIDS SINCE IT IS NOW A BANNED SUBSTANCE FOR ENVIRONMENTAL PROTECTION. FIGURE 1 - CABLE CONFIGURATION 1. CONSTRUCTION DESCRIPTION 1.1 OPTICAL FIBER DIMENSIONS AND MATERIALS CORE DIAMETER: 200 M 4.0 m (0.0078 IN 0.00016 IN) CORE MATERIAL: STEP INDEX SILICA GLASS CLADDIN
7、G DIAMETER: 230 +0, -10 m (0.0091 +0, -0.0004 IN) CLADDING MATERIAL: HARD POLYMER (HCS) CORE TO CLADDING ELLIPTICITY: 3% MAXIMUM CORE TO CLADDING OFFSET: 5 m MAXIMUM HERMETIC COATED: NO PRIMARY COATING: NO AEROSPACE STANDARD AS5382/6SHEET 2 OF 4REV. ACABLE, FIBER OPTIC, MULTI-MODE, 200/230/500 m, ST
8、EP INDEX, TIGHT BUFFER 1.2 CABLE DIMENSIONS AND MATERIALS UPJACKET DIAMETER: 500 m 30 m (0.0195 IN 0.00117 IN) UPJACKET MATERIAL: ETHYLENE-TETRAFLUOROETHYLENE COPOLYMER (ETFE) STRENGTH MEMBER: BRAIDED ARAMID FIBER YARN SIZE: 380 DENIER NUMBER OF ENDS: 16 BRAID PICKS/INCH: 9 OUTER JACKET DIAMETER: 18
9、00 m 100 m (0.0709 IN MAX 0.039 IN MAX) OUTER JACKET MATERIAL: ETHYLENE-TETRAFLUOROETHYLENE COPOLYMER (ETFE) OUTER JACKET CONCENTRICITY: 6% OF JACKET OUTER DIAMETER 1.3 CABLE PERFORMANCE OPERATIONAL MODE: MULTI-MODE TEMPERATURE RATING: -55 TO +125 C STORAGE TEMPERATURE: -55 TO +85 C OUTER JACKET COL
10、OR: PURPLE FINISHED CABLE WEIGHT: 4.0 KG/KM MAXIMUM 2. OPTICAL FIBER REQUIREMENTS MAXIMUM ATTENUATION: d8 DB/KM 850 NM NUMERICAL APERTURE: 0.37 0.02 FIBER TENSILE PROOF TEST: 150,000 PSI MINIMUM BANDWIDTH t20 MHZ-KM 850 NM 3. ENVIRONMENTAL FLUID IMMERSION: SEE TABLE 1 FOR TEST FLUID LISTING. FREEZIN
11、G WATER IMMERSION: d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE DURING THE TEST WITH d0.5 DB PERMANENT CHANGE AFTER TEST HUMIDITY RESISTANCE: d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE DURING THE TEST WITH d0.5 DB PERMANENT CHANGE AFTER TEST WICKING: WATER PENETRATION OF 88.5 MM MAXIMUM FUNGUS RESISTANCE: F
12、UNGUS INERT PER MIL-HDBK-454 GUIDELINE 4 BLOCKING: NO AREAS OF LOCALIZED ADHESION AEROSPACE STANDARD AS5382/6SHEET 3 OF 4REV. ACABLE, FIBER OPTIC, MULTI-MODE, 200/230/500 m, STEP INDEX, TIGHT BUFFER 4. MECHANICAL COLD BEND: d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE AFTER TEST CYCLIC FLEX: d0.5 DB CHAN
13、GE IN OPTICAL TRANSMITTANCE DURING THE TEST WITH d0.5 DB PERMANENT CHANGE AFTER TEST TEST TEMPS: -55 C, +25 C, +125 C IMPACT RESISTANCE: d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE DURING THE TEST WITH d0.5 DB PERMANENT CHANGE AFTER TEST CRUSH RESISTANCE: d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE DURING T
14、HE TEST WITH d0.5 DB PERMANENT CHANGE AFTER TEST CORNER BEND: d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE DURING THE TEST WITH d0.5 DB PERMANENT CHANGE AFTER TEST CABLE TENSILE LOAD AND d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE DURING THE TEST WITH BENDING: d0.5 DB PERMANENT CHANGE AFTER TEST MAXIMUM TENS
15、ILE LOAD 132 N JACKET MATERIAL TENSILE STRENGTH: 900 N/CM2MINIMUM TENSILE AND ELONGATION: ELONGATION: 125% MINIMUM DURABILITY OF MANUFACTURERS REQUIRED UNLESS IDENTIFICATION MARKING IS UNDER A CLEAR JACKET IDENTIFICATION: JACKET STRIPPABILITY: EASILY REMOVED, NO DAMAGE TO FIBER AT 10X 5. THERMAL FLA
16、MMABILITY: AFTER FLAME: 30 SECONDS MAXIMUM FLAME TRAVEL: 3 INCHES MAXIMUM TISSUE FLAMING: NONE THERMAL SHOCK: TEMPERATURE RANGE: -55 TO +125 C MAXIMUM CABLE DIAMETER CHANGE OF 10% d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE AFTER TEST PROPERTY RETENTION 750 H AT 125 C AFTER THERMAL AGING: 300 H AT 130 C
17、 100 H AT 150 C MAXIMUM CABLE DIAMETER CHANGE OF 10% d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE AFTER TEST JACKET TENSILE AND ELONGATION: 75% OF INITIAL VALUE STORAGE LIFE: TEMPERATURE RANGE: -55 TO +85 C NO VISUAL DAMAGE AT 10X MAGNIFICATION d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE AFTER TEST TEMPERATU
18、RE CYCLING: 5 CYCLES, TEMPERATURE RANGE: -55 TO +125 C MAXIMUM CABLE DIAMETER CHANGE OF 10% d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE DURING THE TEST WITH d0.5 DB PERMANENT CHANGE AFTER TEST TEMPERATURE CYCLING 5 CYCLES, TEMPERATURE RANGE: -55 TO +125 C WITH MANDREL: WRAPPED 5 TIMES AROUND A 0.75 INCH
19、 MANDREL MAXIMUM CABLE DIAMETER CHANGE OF 10% d0.5 DB CHANGE IN OPTICAL TRANSMITTANCE DURING THE TEST WITH d0.5 DB PERMANENT CHANGE AFTER TEST JACKET SHRINKAGE: 2.3 MM MAXIMUM IN A 360 MM SAMPLE AEROSPACE STANDARD AS5382/6SHEET 4 OF 4REV. ACABLE, FIBER OPTIC, MULTI-MODE, 200/230/500 m, STEP INDEX, T
20、IGHT BUFFER TABLE 1 - IMMERSION TEST FLUIDS TEST FLUID TEST TEMPERATURE IMMERSION TIME MIL-PRF-23699, Lubricating Oil, Aircraft Turbine Engine, Synthetic Base 48 to 50 C 20 hours MIL-PRF-5606, Hydraulic Fluid, Petroleum Base, Aircraft, Missile and Ordnance 48 to 50 C 20 hours TT-I-735, Isopropyl Alc
21、ohol (Grade A or B) 20 to 25 C 168 hours MIL-DTL-5624, Turbine Fuel, Aviation, Grade JP-4 and JP-5 20 to 25 C 168 hours SAE AMS 1424, Deicing/Anti-Icing Fluid, Aircraft, SAE Type I 48 to 50 C 20 hours SAE AMS 1432, Fluid, Deicing/Anti-Icing, Runways and Taxiways, Potassium Acetate Base 48 to 50 C 20
22、 hours MIL-C-43616, Cleaning Compound, Aircraft Surface 48 to 50 C 20 hours ASTM D 1153, Methyl Isobutyl Ketone (for use in Organic Coatings) 20 to 25 C 168 hours MIL-PRF-7808, Lubricating Oil, Aircraft Turbine Engine, Synthetic Base 118 to 121 C 30 minutes MIL-PRF-85570, Type 3 Cleaning Compound, A
23、lkaline 63 to 68 C 20 hours MIL-PRF-87252, Coolant Fluid, Hydrolytically Stable, Dielectric (POA) 20 to 25 C 168 hours MIL-DTL-83133, Turbine Fuel, Aviation Grade, JP-8 20 to 25 C 168 hours MIL-PRF-83282, Hydraulic Fluid 48 to 50 C 20 hours Halon Bromotrifluoromethane (CFBR) Gas at -76 C 48 to 50 C
24、168 hours Halon Bromotrifluoromethane (CFBR) Gas at -76 C -55 to -65 C 168 hours NOTES: A CHANGE BAR ( L ) LOCATED IN THE LEFT MARGIN IS FOR THE CONVENIENCE OF THE USER IN LOCATING AREAS WHERE TECHNICAL REVISIONS, NOT EDITORIAL CHANGES, HAVE BEEN MADE TO THE PREVIOUS ISSUE OF THIS DOCUMENT. AN (R) SYMBOL TO THE LEFT OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION OF THE DOCUMENT, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS, NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY.
