1、AEROSPACE STANDARD (R) CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, SHIELDED (FOR MIL-DTL-26500AND MIL-DTL-26518 CONNECTORS) AS39029/54Copyright 2010 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any for
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3、:/www.sae.org ISSUED 2000-07REAFFIRMED 2007-01 REVISED 2010-11THIRD ANGLE PROJECTION CUSTODIAN: AE-8C1 REV.AFEDERAL SUPPLY CLASS 5935 AS39029/54SHEET 1 OF 4REV. APROCUREMENT SPECIFICATION: AS39029SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of t
4、echnicalandengineering sciences. Theuse ofthis report 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 itm
5、ay bereaffirmed, revised, orcancelled. SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS39029/54ARATIONALE REVISE TO INCLUDE COMMENTS RECEIVED BY THE GOVERNMENT AND INDUSTRY, REMOV
6、E GOVERNMENT JARGON, ADD QUALIFICATION REQUIREMENTS, UPDATE REFERENCES, ALIGN SPECIFICATION WITH SAE GUIDELINES, AND REVIEW SPECIFICATION FOR KNOWN TECHNICAL PROBLEMS. NOTICE THE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS SPECIFICATION SHEET AND THE LATEST ISSUE OF
7、 SAE AS39029. FIGURE 1 CONNECTOR CONTACT Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/54SHEET 2 OF 4REV. A(R) CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, SHIEL
8、DED (FOR MIL-DTL-26500 AND MIL-DTL-26518 CONNECTORS) FIGURE 2 BOOT, SEALING FIGURE 3 SLEEVE, SEALING, COAXIAL CABLE TABLE 1 DIMENSIONS BIN CODE A(REF) BMAXCDDIAEDIAFDIAGDIAHMAXDIANDIAP342.865(21.97) .298(7.57) .062(1.57) .044(1.12) .124(3.15) .122(3.10) .161(4.09) .158(4.01) .135(3.43) .131(3.33) .2
9、02(5.13) .196(4.98) .154(3.91) .028(.71) .026(.66) .066 (1.68) .020 (.51) 343.865(21.97) .298(7.57) .050(1.27) .044(1.12) .215(5.46) .213(5.41) .252(6.40) .249(6.32) .226(5.74) .221(5.61) .313(7.95) .309(7.85) .195(4.95) .045(1.14) .043(1.09) .016 (.41) RECESSED.010 (.25) PROTRUSION TABLE 2 DESIGN C
10、HARACTERISTICS BIN CODE COLOR BANDS CONTACT CAVITY SIZECABLEACCOMMODATED TYPE CLASS 1ST 2ND 3RD 342 ORANGE YELLOW RED 12 M27500-22RE1N06 D A 343 ORANGE YELLOW ORANGE 8 M27500-20RE1N06 Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permit
11、ted without license from IHS-,-,-AEROSPACE STANDARD AS39029/54SHEET 3 OF 4REV. A(R) CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, SHIELDED (FOR MIL-DTL-26500 AND MIL-DTL-26518 CONNECTORS) TABLE 3 TOOLS BIN CODE INNER CONTACT OUTER CONTACT INSTALLING TOOL 1/REMOVAL TOOL 1/BASIC CRIMPING TOOL
12、POSITIONER BASIC CRIMPING TOOL CRIMPING DIE 342 M22520/2-01 M22520/2-33 M22520/5-01 M22520/10-01 M22520/5-08 M22520/10-05(A)M81969/17-05 M81969/19-09 343 M22520/2-01 M22520-2-24 M22520/5-01 M22520/10-01 M22520/5-10 M22520/10-06 M81969/17-06 M81969/19-03 1/ INSTALLING AND REMOVAL TOOLS SHOWN ARE FOR
13、MIL-DTL-26500 CONNECTOR APPLICATIONS. WHEN THESE CONTACTS ARE USED IN OTHER APPLICATIONS, USE CONNECTOR MANUFACTURERS RECOMMENDATION FOR INSTALLING AND REMOVAL TOOLS. TABLE 4 PART NUMBER BIN CODE PART NUMBER SUPERSEDED PART NUMBER 342 M39029/54-342 MS27184-22P343 M39029/54-343 MS27184-20P REQUIREMEN
14、TS: ALL REQUIREMENTS SHALL CONSIST OF THIS SPECIFICATION AND THE LATEST ISSUE OF AS39029. 1. DESIGN: CONTACTS SHALL BE DESIGNED IN ACCORDANCE WITH FIGURES 1, 2 AND 3, AND TABLES 1 AND 2. DIMENSIONS ARE IN INCHES, METRIC EQUIVALENTS ARE GIVEN FOR GENERAL INFORMATION ONLY. DIMENSIONS SHOWN APPLY AFTER
15、 PLATING. BOOT SEALING: ALL DIMENSIONS ARE AFTER CURING, ALL DIAMETERS SHALL BE CONCENTRIC WITHIN .004 T.I.R. RADII SHALL BE .008 MAXIMUM UNLESS OTHERWISE SPECIFIED. SLEEVE SEALING: COLOR, WHITE. 2. TOOLS: TOOLS REQUIRED FOR CRIMPING CONTACTS TO WIRE/CABLE AND THE INSTALLING/REMOVAL FROM THE CONNECT
16、OR SHALL BE IN ACCORDANCE WITH TABLE 3. 3. PART NUMBERS: CONTACT PART NUMBERS SHALL BE IN ACCORDANCE WITH TABLE 4. SUPERSEDED PART NUMBERS ARE AS SPECIFIED. 4. MATERIALS: MATERIALS AND PLATING SHALL BE IN ACCORDANCE WITH AS39029. BOOTS AND SLEEVE SEALING: PARTS MUST BE FREE OF FLASH, CRACKS OR CAVIT
17、IES (SEE FIGURE 2), BOOTS SEALING: IMMEDIATELY AFTER MOLDING, CURE BOOTS, SLEEVE SEALING MATERIAL: FLEXITE SR200 SILICONE RUBBER EXTRUDED TUBING PER A-A-59588 CLASS 2B, OR EQUIVALENT STANDARD WALL (SEE FIGURE 3). 5. MECHANICAL: MECHANICAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029. 6. ELECTRICAL
18、: ELECTRICAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/54SHEET 4 OF 4REV. A(R) CONTACTS, ELECTRICAL CONNECTOR, PIN, CR
19、IMP REMOVABLE, SHIELDED (FOR MIL-DTL-26500 AND MIL-DTL-26518 CONNECTORS) 7. ENVIRONMENTAL: ENVIRONMENTAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029. VIBRATION: IN ACCORDANCE WITH EIA-364-28, TEST CONDITION IV. SHOCK (SPECIFIED PULSE): IN ACCORDANCE WITH EIA-364-27, TEST CONDITION C. THE FORCES S
20、HALL BE PRODUCED BY SECURING THE CONNECTORS TO A SUFFICIENT MASS AND DROPPING THE ASSEMBLY THROUGH SUCH A HEIGHT THAT WHEN DECELERATED BY RESILIENT IMPACT, A FORCE OF 100 GRAVITY UNITS IS OBTAINED AS OUTLINED IN MIL-STD-202, METHOD 213, TEST CONDITION C. AT LEAST ONE BLOW SHALL BE APPLIED IN EACH MA
21、JOR AXIS OF THE CONNECTOR SO THAT THE RESULTANT FORCE TENDS TO DISENGAGE THE CONNECTORS. RECEPTACLES SHALL BE MOUNTED BY A METHOD SIMILAR TO THE VIBRATION TEST ON THE SHOCK DEVICE OR CARRIAGE. PLUGS SHALL BE ENGAGED WITH THE RECEPTACLES. THE CONNECTORS SHALL BE WIRED IN SERIES WITH AT LEAST 100 MILL
22、IAMPERES ALLOWED TO FLOW. THE WIRE BUNDLE OR CABLE SHALL BE CLAMPED TO POINTS THAT MOVE WITH THE CONNECTOR. A MINIMUM OF 8 INCHES OF WIRE OR CABLE SHALL BE UNSUPPORTED BEHIND EACH CONNECTOR.8. PACKAGING: BOOTS AND SEALING SLEEVE (FIGURES 2 AND 3) SHALL BE SHIPPED WITH UNIT PACKAGE. MANUFACTURERS REC
23、OMMENDED ASSEMBLY INSTRUCTIONS SHALL ALSO BE SHIPPED WITH UNIT PACKAGE. APPLICATION NOTES: 1. CONTACT MATES DIRECTLY WITH AN AS39029/55 SOCKET CONTACT AS SHOWN IN TABLE 5. TABLE 5. CONTACT MATING PART NUMBERS AS39029/54 BIN CODE MATING AS39029 SLASH SHEET/BIN CODE -342 M39029/55-344-343 M39029/55-34
24、51. SPECIFICATION NOTES: A CHANGE BAR (|) 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 REVIS
25、ION OF THE DOCUMENT, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ORIGINAL PUBLICATIONS NOR IN DOCUMENTS THAT CONTAIN EDITORIAL CHANGES ONLY. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
