1、AEROSPACE STANDARD CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR MIL-DTL-28840 CONNECTORS) AS39029/84Copyright 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, electroni
2、c, mechanical, 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 2000-07
3、REVISED 2011-02THIRD ANGLE PROJECTION CUSTODIAN: AE-8/AE-8C1 REV.AFEDERAL SUPPLY CLASS 5935 AS39029/84SHEET 1 OF 4REV. APROCUREMENT SPECIFICATION: AS39029SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse of
4、this 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 itmay bereaffirmed, revised, orcancelled. SAE
5、 invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS39029/84ARATIONALE REVISE TO INCLUDE COMMENTS RECEIVED BY THE GOVERNMENT AND INDUSTRY, REMOVE GOVERNMENT JARGON, ADD QUALIFICATION REQ
6、UIREMENTS, 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 SAE AS39029. FIGURE 1 DIMENSIONS AND CONF
7、IGURATION Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/84SHEET 2 OF 4REV. ACONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR MIL-DTL-28840 CONNECTORS) TABLE 1
8、 - DESIGN CHARACTERISTICS BINCODE BDIA.COLOR BANDS MATINGEND SIZEWIREBARRELSIZETYPE CLASS C 1/DIA.1ST2ND3RD509.050(1.27) .048(1.22) GREEN BLACK WHITE 20 20 A B .032(.813).026(.660) 452.0355(.902) .0335(.851) YELLOW GREEN RED 20 22 A B .032(.813).026(.660) 453.0200(.508) .0180(.457) YELLOW GREEN ORAN
9、GE 20 28 A B .022(.559).018(.457) 1/ HOLE ONE WALL. TABLE 2 TOOLS BIN CODE BASIC CRIMPING TOOL POSITIONER INSTALLING TOOL REMOVAL TOOL 509 M22520/34-01 M22520/34-02 M81969/33-01 M81969/34-01 452 M22520/34-01 M22520/34-02 M81969/33-01 M81969/34-01 453 M22520/34-01 M22520/34-02 M81969/33-01 M81969/34-
10、01 TABLE 3 PART NUMBER AND BIN CODE PART NUMBER BIN CODE SUPERSEDED PART NUMBER M39029/84-509 509 - M39029/84-452 451 M39029/84-20-22 M39029/84-453 452 M39029/84-20-28 TABLE 4 LOW SIGNAL LEVEL CONTACT RESISTANCE (TYPE A) MATINGENDSIZEWIREBARRELSIZEWIRESIZEMAXIMUM CONTACT RESISTANCE (MILLIOHMS) INITI
11、AL AFTERCONDITIONING 20 20 2024920112320 22 22261531173820 28 283050756088Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/84SHEET 3 OF 4REV. ACONTACTS, ELECTRICAL CONNECTOR
12、 SOCKET, CRIMP REMOVABLE (FOR MIL-DTL-28840 CONNECTORS) TABLE 5 CONTACT RESISTANCE (TYPE A) WITH SILVER PLATED WIRE MATINGENDSIZEWIREBARRELSIZEWIRESIZERANGE TESTCURRENT (AMPERES)MAXIMUM VOLTAGE DROP (MILIVOLTS) 25 C 3 C 25 C 3 C AFTERCONDITIONING 200 C +3 C -0 C MAX MAX AVGMAX MAXAVG. MAX MAX AVG.
13、20 20 20247.5355455041665456469477716320 22 22265.02.0735366488864755512591 946920 28 28301.51.05460495565735662921036978TABLE 6 TENSILE STRENGTH (TYPE A) MATINGENDSIZEWIREBARRELSIZEWIRESIZEAXIAL LOAD (POUNDS) SILVER TIN-PLATED COPPER WIRES NICKEL-PLATED COPPER WIREHIGHSTRENGTH COPPER ALLOY WIRE INI
14、TIALCONDITION VALUESTHERMALCONDITION VALUESINITIALCONDITION VALUESTHERMALCONDITION VALUESINITIALCONDITION VALUES20 20 202420814619614.34.5- 20 22 22261257.54.0836.02.5221020 28 283031.52.251.1321.51.501.135.53.4REQUIREMENTS: ALL REQUIREMENTS SHALL CONSIST OF THIS SPECIFICATION AND THE LATEST ISSUE O
15、F AS39029. 1. DESIGN: CONTACTS SHALL BE DESIGNED IN ACCORDANCE WITH FIGURE 1 AND TABLE 1. DIMENSIONS ARE IN INCHES. METRIC EQUIVALENTS ARE GIVEN FOR GENERAL INFORMATION ONLY. DIMENSIONS SHOWN APPLY AFTER PLATING. THE .290 MIN DIMENSION IS THE CONTACT ENGAGEMENT AREA FOR LOCALIZED FINISH OPTION (SEE
16、REQUIREMENTS). 2. TOOLS: TOOLS REQUIRED FOR CRIMPING CONTACTS TO WIRE/CABLE AND THE INSTALLING/REMOVAL FROM THE CONNECTOR SHALL BE IN ACCORDANCE WITH TABLE 2. 3. PART NUMBERS: CONTACT PART NUMBERS SHALL BE IN ACCORDANCE WITH TABLE 3. SUPERSEDED PART NUMBERS ARE AS SPECIFIED. Copyright SAE Internatio
17、nal Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/84SHEET 4 OF 4REV. ACONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE (FOR MIL-DTL-28840 CONNECTORS) 4. MATERIALS: MATERIALS AND PLATING SHALL
18、 BE IN ACCORDANCE WITH AS39029. LOCALIZED FINISH OPTION: APPLICABLE CONTACTS SHALL BE FURNISHED AS SPECIFIED IN THE LOCALIZED FINISH REQUIREMENTS OF AS39029. THE 0.290 INCH MINIMUM LENGTH REQUIREMENT IN THE FIGURE IS THE “F” LENGTH OF THE AREA “X” SPECIFIED IN AS39029 FOR CONTACTS HAVING SEPARATE PR
19、ESSURE MEMBERS. 5. MECHANICAL: MECHANICAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029. TENSILE STRENGTH (TYPE A): SEE TABLE 6. 6. ELECTRICAL: ELECTRICAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029. LOW SIGNAL LEVEL CONTACT RESISTANCE (TYPE A): SEE TABLE 4. CONTACT RESISTANCE (TYPE A) WITH SILV
20、ER PLATED WIRE: SEE TABLE 5. 7. ENVIRONMENTAL: ENVIRONMENTAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029. VIBRATION: IN ACCORDANCE WITH EIA-364-28, TEST CONDITION III, FOLLOWING THE TEST, THE CONTACTS SHALL BE TESTED FOR ENDURANCE IN ACCORDANCE WITH MIL-STD-167-1. ALL CONTACTS SHALL BE WIRED IN S
21、ERIES. THE ELECTRICAL LOAD CONDITION SHALL BE 100 10 MILLIAMPERES. HIGH IMPACT SHOCK: HIGH IMPACT SHOCK TEST SHALL BE CONDUCTED IN ACCORDANCE WITH MIL-DTL-28840, USING A MIL-DTL-28840 QUALIFIED CONNECTOR THAT HAS BEEN APPROVED FOR LISTING ON THE APPLICABLE QUALIFIED PRODUCTS LIST. APPLICATION NOTES:
22、 1. CONTACT MATES DIRECTLY WITH AN AS39029/83 PIN CONTACT AS SHOWN IN TABLE 7. TABLE 7. CONTACT MATING PART NUMBERS AS39029/84 BIN CODE MATING AS39029 SLASH SHEET/BIN CODE -509 M39029/83-508-452 M39029/83-450-453 M39029/83-4511. SPECIFICATION NOTES: A CHANGE BAR (|) LOCATED IN THE LEFT MARGIN IS FOR
23、 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. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
