1、AEROSPACE STANDARD CABLE, FIBER OPTIC, MULTIMODE, 100/140/172 m GRADED INDEX, NONHERMETIC, LOOSE TUBE AS5382/2Copyright 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, mec
2、hanical, photocopying, 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 2004-08REVISE
3、D 2011-10THIRD ANGLE PROJECTION CUSTODIAN: AE-8/AE-8D REV.AFEDERAL SUPPLY CLASS 6010 AS5382/2SHEET 1 OF 3REV. APROCUREMENT SPECIFICATION: NONESAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse ofthis report
4、is entirely 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 you
5、rwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS5382/2ARATIONALE THIS DOCUMENT IS OVERDUE FOR ITS FIVE YEAR REVIEW AND REVIEW OF THE DOCUMENT NECESSITATES ELIMINATION OF ONE FLUID,1,1,1 TRICHLOR
6、OETHANE, FROM 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: 100 r 4PM (0.0039 r 0.00016 IN.) CORE MATERIAL: GRADED INDEX SILICA GL
7、ASS CLADDING DIAMETER: 140 r 3PM (0.0055 r 0.00012 IN.) CLADDING MATERIAL: SILICA GLASS CORE/CLADDING CONCENTRICITY: 0.94 MINIMUM HERMETIC COATED: NO COATING DIAMETER: 172 r 2PM (0.00677 r 0.00008 IN.) COATING MATERIAL: POLYIMIDE CLADDING/COATING CONCENTRICITY: 0.82 MINIMUM 1.2 CABLE DIMENSIONS AND
8、MATERIALS BUFFER: LOOSE TUBE INNER DIAMETER: 0.38 r 0.025 MM (0.0150 r 0.001 IN.) OUTER DIAMETER: 0.76 r 0.025 MM (0.0300 r 0.001 IN.) BUFFER MATERIAL: FEP STRENGTH MEMBER: BRAIDED PTFE-COATED FIBERGLASS COVERAGE: 90% MINIMUM OUTER DIAMETER: 1.60r .051 MM (.0630r .002IN.) OUTER JACKET DIAMETER: 2.11
9、 r 0.05 MM (0.083 r 0.002 IN.) OUTER JACKET MATERIAL: EXTRUDED FLUORINATED ETHYLENE PROPYLENE (FEP) AEROSPACE STANDARD AS5382/2SHEET 2 OF 3REV. ACABLE, FIBER OPTIC, MULTIMODE, 100/140/172 m GRADED INDEX, NONHERMETIC, LOOSE TUBE 1.3 CABLE PERFORMANCE OPERATIONAL MODE: MULTIMODE TEMPERATURE RATING: -6
10、5 qC TO +200 qCSTORAGE TEMPERATURE: -55 qC TO +200 qCOUTER JACKET COLOR: VIOLET (NON-STANDARD COLOR) BRAID BREAK FORCE: 80 LBS. MINIMUM FINISHED CABLE WEIGHT: 5.95 KG/KM (4.0 LBS./1000 FEET) MAXIMUM MINIMUM BEND RADIUS: 0.85 IN. (10X OD) 2. OPTICAL FIBER REQUIREMENTS MAXIMUM ATTENUATION: d10DB/KM 76
11、0 - 992 NM NUMERICAL APERTURE: 0.29 r 0.020 FIBER TENSILE PROOF TEST: 200 000 PSI MINIMUM BANDWIDTH: 100 MHZ-KM MIN. 850NM & 1300NM 3. ENVIRONMENTAL FLUID IMMERSION: SEE TABLE 1 FOR TEST FLUID LISTING. FREEZING WATER IMMERSION: d0.5DB CHANGE IN OPTICAL TRANSMITTANCE DURING & AFTER TEST HUMIDITY RESI
12、STANCE: d0.5DB CHANGE IN OPTICAL TRANSMITTANCE DURING & AFTER TEST WICKING: WATER PENETRATION OF 88.5MM MAXIMUM FUNGUS RESISTANCE: FUNGUS INERT PER MIL-HDBK-454 GUIDELINE 4 BLOCKING: NO AREAS OF LOCALIZED ADHESION 4. MECHANICAL COLD BEND: d0.5DB CHANGE IN OPTICAL TRANSMITTANCE AFTER TEST CYCLIC FLEX
13、 d0.5DB CHANGE IN OPTICAL TRANSMITTANCE DURING & AFTER TEST TEST TEMPS: -55 qC, +25 qC, +150 qCIMPACT RESISTANCE: d0.5DB CHANGE IN OPTICAL TRANSMITTANCE AFTER TEST CRUSH RESISTANCE: d0.5DB CHANGE IN OPTICAL TRANSMITTANCE DURING & AFTER TEST CORNER BEND: d0.5DB CHANGE IN OPTICAL TRANSMITTANCE AFTER
14、TEST CABLE TENSILE LOAD AND d0.5DB CHANGE IN OPTICAL TRANSMITTANCE DURING & AFTER TEST BENDING: MAXIMUM TENSILE LOAD 35 000 PSI. JACKET MATERIAL TENSILE STRENGTH: 5,000 PSI MINIMUM TENSILE AND ELONGATION: ELONGATION: 200% MINIMUM DURABILITY OF MANUFACTURERS REQUIRED UNLESS IDENTIFICATION MARKING IS
15、UNDER A CLEAR JACKET IDENTIFICATION: JACKET STRIPPABILITY: EASILY REMOVED, NO DAMAGE TO STRENGTH MEMBER. AEROSPACE STANDARD AS5382/2SHEET 3 OF 3REV. ACABLE, FIBER OPTIC, MULTIMODE, 100/140/172 m GRADED INDEX, NONHERMETIC, LOOSE TUBE 5. THERMAL FLAMMABILITY: AFTER FLAME: 30 SECONDS MAXIMUM FLAME TRAV
16、EL: 3 INCHES MAXIMUM TISSUE FLAMING: NONE THERMAL SHOCK: TEMPERATURE RANGE: -55 qC TO +200 qCMAXIMUM CABLE DIAMETER CHANGE OF r10% d0.5DB CHANGE IN OPTICAL TRANSMITTANCE AFTER TEST PROPERTY RETENTION 750 HRS.180 qC, AFTER THERMAL AGING: 300 HRS.200 qC, 100 HRS.220 qCMAXIMUM CABLE DIAMETER CHANGE OF
17、r10% d0.5DB CHANGE IN OPTICAL TRANSMITTANCE AFTER TEST JACKET TENSILE AND ELONGATION: 75% OF INITIAL VALUE STORAGE LIFE: TEMPERATURE RANGE: -55 qC TO +200 qCNO VISUAL DAMAGE AT 10X MAGNIFICATION d0.5DB CHANGE IN OPTICAL TRANSMITTANCE AFTER TEST TEMPERATURE CYCLING: 5 CYCLES, TEMPERATURE RANGE: -55 q
18、C TO +200 qCMAXIMUM CABLE DIAMETER CHANGE OF r10% d0.5DB CHANGE IN OPTICAL TRANSMITTANCE DURING TEST AT TEMPERATURE EXTREMES AND AFTER TEST JACKET SHRINKAGE: 1/16 INCH MAXIMUM (TOTAL FOR BOTH ENDS) IN A 6.6 FT SAMPLE TABLE 1 - IMMERSION TEST FLUIDS TEST FLUID TEST TEMPERATURE IMMERSION TIME MIL-PRF-
19、23699, Lubricating Oil, Aircraft Turbine Engine, Synthetic Base 48 TO 50 qC 20 HOURS MIL-PRF-5606, Hydraulic Fluid, Petroleum Base, Aircraft, Missile and Ordnance 48 TO 50 qC 20 HOURS TT-I-735, Isopropyl Alcohol (Grade A or B) 20 TO 25 qC 168 HOURS MIL-DTL-5624, Turbine Fuel, Aviation, Grade JP-4 an
20、d JP-5 20 TO 25 qC 168 HOURS SAE AMS 1424, Anti Icing and Deicing-Defrosting Fluid,Undiluted and 60/40 Fluid/Water Dilution 48 TO 50 qC 20 HOURS MIl-C-43616, Cleaning Compound, Aircraft Surface 48 TO 50 qC 20 HOURS ASTM D 1153, Methyl Isobutyl Ketone 20 TO 25 qC 168 HOURS MIL-H-83306, Hydraulic Flui
21、d, Phosphate Ester Base 48 TO 50 qC 20 HOURS MIL-PRF-7808, Lubricating Oil, Aircraft Turbine Engine, Synthetic Base 118 TO 121 qC 5 MINUTES MIL-C-87937, Cleaning Compound, Aircraft Surface, Type 2 or Type 4 Undiluted and Diluted with 5 Parts Water 63 TO 68 qC 20 HOURS ASTM D471, Ref. Fuel A 20 TO 25
22、 qC 168 HOURS ASTM D471, Ref. Fuel D 20 TO 25 qC 168 HOURS ASTM D471, Ref. Oil 1 20 TO 25 qC 168 HOURS Dielectric Coolant Fluid, Synthetic, Silicate, Ester Base, “Coolanol 25” or equivalent 20 TO 25 qC 168 HOURS PAO “Royco 602” or equivalent 20 TO 25 qC 168 HOURS MIL-DTL-83133 Turbine Fuel, Aviation
23、 Grade, JP-8 20 TO 25 qC 168 HOURS NOTES A CHANGE BAR (I) 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.
