1、AEROSPACE STANDARD (R) CONTACTS, ELECTRICAL CONNECTOR SOCKET, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL-38999 SERIES I, III, IV CONNECTORS) AS39029/88Copyright 2009 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in
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3、S: http:/www.sae.org ISSUED 2000-07REAFFIRMED 2006-10 REVISED 2009-09THIRD ANGLE PROJECTION CUSTODIAN: AE-8C1 REV.AFEDERAL SUPPLY CLASS 5999 AS39029/88SHEET 1 OF 6REV. APROCUREMENT SPECIFICATION: AS39029SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thesta
4、te of technicalandengineering 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 t
5、ime itmay 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/AS39029/88ARATIONALE REVISE TO INCLUDE COMMENTS RECEIVED BY THE GOVERNMENT AND INDUSTRY
6、, REMOVE GOVERNMENT JARGON, 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 -
7、SOCKET CONTACTS (SEE DESIGN PARAGRAPH FOR ADDITIONAL DIMENSIONAL DETAILS). Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/88SHEET 2 OF 6REV. A(R) CONTACTS, ELECTRICAL CONN
8、ECTOR SOCKET, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL-38999 SERIES I, III, IV CONNECTORS) TABLE 1 - CONTACT DIMENSIONS BIN CODE A DIA B DIA C DIA D DIA E DIA F DIA MAX G H J K M N P DIA MIN482THROUGH 485.855(21.72).031(.79)MIN.062(1.57).060(1.52) .022(.56).018(.46) .0355(.90).0335(.85) .062(1.57)
9、 .048(1.22).046(1.17) .005(.13).003(.08) .626(15.90) .616(15.65) .141(3.58)MINN/A5044 .047(1.19) 486THROUGH 489.044(1.12).042(1.07) .094(2.39).091(2.31) .032(.81).026(.66) .048(1.22).046(1.17) .078(1.98) .070(1.78).068(1.73) .010(.25).005(.13) .229(5.87).209(5.31) .078(1.98).072(1.83) 4740 .053(1.35
10、) 490THROUGH 493.064(1.63)MIN.130(3.30).127(3.23) .042(1.07).036(.914) .068(1.73).066(1.68) .113(2.87) .103(2.62).101(2.57) .088(2.24).082(2.08) .084(2.13) TABLE 2 - MARKING AND DESIGN CHARACTERISTICS BINCODE COLOR BANDS MATINGEND SIZEWIREBARRELLSIZETYPE CLASS 1ST2ND3RD482 YELLOW GRAY RED 22 22D C(S
11、EE TABLE 4) B483 YELLOW GRAY ORANGE 22 22D 484 YELLOW GRAY YELLOW 22 22D 485 YELLOW GRAY GREEN 22 22D 486 YELLOW GRAY BLUE 20 20 487 YELLOW GRAY VIOLET 20 20 488 YELLOW GRAY GRAY 20 20 489 YELLOW GRAY WHITE 20 20 490 YELLOW WHITE BLACK 16 16 491 YELLOW WHITE BROWN 16 16 492 YELLOW WHITE RED 16 16 49
12、3 YELLOW WHITE ORANGE 16 16 Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/88SHEET 3 OF 6REV. A(R) CONTACTS, ELECTRICAL CONNECTOR SOCKET, CRIMP REMOVABLE, THERMOCOUPLE (FO
13、R MIL-DTL-38999 SERIES I, III, IV CONNECTORS) TABLE 3 - TOOLS BIN CODE BASIC CRIMPING TOOL POSITIONER INSTALLING TOOL REMOVAL TOOL 482, 483, 484, 485 M22520/2-01 OR M22520/7-01 M22520/2-07 OR M22520/7-05 M81969/8-01 OR M81969/14-01 M81969/8-02 OR M81969/14-01 486, 487, 488, 489 M22520/1-01 OR M22520
14、/2-01 OR M22520/7-01 M22520/1-04 OR M22520/2-10 OR M22520/7-08 M81969/8-05 OR M81969/14-02 M81969/8-06 OR M81969/14-02 490, 491, 492, 493 M22520/1-01 OR M22520/7-01 M22520/1-04 OR M22520/7-04 M81969/8-07 OR M81969/14-03 M81969/8-08 OR M81969/14-03 TABLE 4 - MATERIALS, PLATING, AND TENSILE STRENGTH B
15、IN CODE MATERIALS PLATING TENSILE STRENGTH 1/WIRE SIZE AXIAL LOAD WIRE SIZE AXIAL LOAD 482 JN NONE 28 MIN 2.25 22 MAX 7.5 483 KN NONE 484 KP NONE 485 JP CADMIUM PLATE 2/486 JN NONE 24 MIN 6.00 20 MAX 12 487 KN NONE 488 KP NONE 489 JP CADMIUM PLATE 2/490 JN NONE 20 MIN 14.00 16 MAX 45 491 KN NONE 492
16、 KP NONE 493 JP CADMIUM PLATE 2/1/ APPLIES TO TYPE 1 WIRE PER MIL-DTL-5846 2/ CHROMATE CLEAR COAT Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/88SHEET 4 OF 6REV. A(R) CO
17、NTACTS, ELECTRICAL CONNECTOR SOCKET, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL-38999 SERIES I, III, IV CONNECTORS) TABLE 5 - PART NUMBER AND BIN CODE PART NUMBER BIN CODE SUPERSEDED M39029/88-482 482 M39029/882222C1 M39029/88-483 483 M39029/882222C2 M39029/88-484 484 M39029/882222C3 M39029/88-485 4
18、85 M39029/882222C4 M39029/88-486 486 1/ M39029/882020C1 M39029/88-487 487 1/ M39029/882020C2 M39029/88-488 488 1/ M39029/882020C3 M39029/88-489 489 1/ M39029/882020C4 M39029/88-490 490 1/ M39029/881616C1 M39029/88-491 491 1/ M39029/881616C2 M39029/88-492 492 1/ M39029/881616C3 M39029/88-493 493 1/ M
19、39029/881616C4 1/ NOT FOR USE WITH MIL-DTL-83733 OR MIL-DTL-24308 CONNECTORS (FOR MIL-DTL-83733 CONTACT SIZES 20 AND 16, SEE AS39029/9). REQUIREMENTS: ALL REQUIREMENTS SHALL CONSIST OF THIS SPECIFICATION AND THE LATEST ISSUE OF AS39029. 1. DESIGN; CONTACTS SHALL BE DESIGNED IN ACCORDANCE WITH FIGURE
20、 1, TABLES 1 AND 2. DIMENSIONS ARE IN INCHES, METRIC EQUIVALENTS ARE GIVEN FOR GENERAL INFORMATION ONLY. DIMENSIONS SHOWN APPLY AFTER PLATING. FOR SIZE 22D ONLY, DIAMETERS E AND G ARE TO BE CONCENTRIC WITHIN .003 (TIR) REGARDLESS OF FEATURE SIZE (RFS); FOR ALL OTHER CONTACT SIZES, DIAMETERS E AND G
21、TO BE CONCENTRIC WITHIN .001 (TIR) AT MAXIMUM MATERIAL CONDITION (MMC). THE .585 MIN DIMENSION IS THE POINT AT WHICH A SQUARE ENDED PIN OF THE SAME BASIC DIAMETER AS THE MATING CONTACT FIRST ENGAGES THE SOCKET CONTACT SPRING. THE .029-.033 DIMENSION IS NOT APPLICABLE FOR SIZE 22D. HOODS SHALL NOT EX
22、CEED CONTACT BODY DIAMETER REGARDLESS OF FEATURE SIZE (RFS) IN ATTACHMENT AREA. 2. TOOLS: TOOLS REQUIRED FOR CRIMPING CONTACTS TO THE WIRE/CABLE AND THE INSTALLING/REMOVAL FROM THE CONNECTOR SHALL BE IN ACCORDANCE WITH TABLE 3. 3. PART NUMBERS: CONTACT PART NUMBERS SHALL BE IN ACCORDANCE WITH TABLE
23、5. SUPERSEDING PART NUMBERS ARE AS SPECIFIED. 4. MATERIALS AND PLATING: SEE TABLE 4 5. TENSILE STRENGTH: SEE TABLE 4. 6. RANDOM VIBRATION: CONNECTORS/CONTACTS SHALL BE TESTED IN ACCORDANCE WITH EIA-364-28 THE FOLLOWING DETAILS SHALL APPLY: a. TEST CONDITION V USING THE VIBRATION ENVELOPE SHOWN IN FI
24、GURE 2. (DERIVED FROM ZONE 2 OUTLINED IN AEROSPACE INFORMATION REPORT AIR1557.) b. VIBRATION TO BE CONDUCTED AT STANDARD TEST CONDITIONS. c. DURATION SHALL BE 8 HOURS IN THE LONGITUDINAL DIRECTION AND 8 HOURS IN A PERPENDICULAR DIRECTION FOR A TOTAL OF 16 HOURS. Copyright SAE International Provided
25、by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/88SHEET 5 OF 6REV. A(R) CONTACTS, ELECTRICAL CONNECTOR SOCKET, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL-38999 SERIES I, III, IV CONNECTORS) FIGURE 2 - VIBRATIO
26、N ENVELOPE 7. HIGH-IMPACT SHOCK: CONNECTORS SHALL BE COUPLED TOGETHER BY NORMAL COUPLING MEANS. ALL CONNECTORS SHALL BE WIRED IN A SERIES CIRCUIT WITH 100 MILLIAMPERES MAXIMUM CURRENT FLOW THROUGH THE SERIES CIRCUIT DURING HIGH-IMPACT SHOCK. CONNECTORS SHALL BE MONITORED FOR ANY DISCONTINUITIES. A D
27、ETECTOR CAPABLE OF DETECTING ALL DISCONTINUITIES IN EXCESS OF 1 MICROSECOND SHALL BE USED. WIRED AND MATED CONNECTORS SHALL BE SUBJECTED TO THE TEST SPECIFIED IN MIL-S-901, GRADE A WITH THE FOLLOWING MODIFICATIONS AND ADDITIONS. MOUNTING FIXTURE SHALL BE IN ACCORDANCE WITH MIL-S-901, LIGHT WEIGHT. T
28、HE CABLE OR WIRE BUNDLE SHALL BE SUPPORTED ON A STATIONARY FRAME IN SUCH A MANNER TO PROVIDE A FREE FLEXING CABLE LENGTH BETWEEN FRAME AND FIXTURE OF NOT LESS THAN 36 INCHES (914.4 MM). TEST CONDITION A. THE PLUG SHALL BE TERMINATED WITH AT LEAST 80 PERCENT OF WIRED CONTACTS. THE WIRE BUNDLE SHALL B
29、E PROVIDED WITH STRAIGHT, OPEN FRAME, STRAIN RELIEF ACCESSORY HARDWARE. 8. QUALIFICATION: THE MANUFACTURERS RELIABILITY ASSURANCE PROGRAM SHALL COMPLY WITH THE AS9100 AEROSPACE STANDARD FOR QUALITY MANAGEMENT SYSTEM REQUIREMENTS. OTHER ESTABLISHED AND INDUSTRY RECOGNIZED QUALITY ASSURANCE STANDARDS
30、THAT ASSURE ALL PRODUCTS PRODUCED CONFORM TO THE CONTRACT REQUIREMENTS ARE ACCEPTABLE. HOWEVER, IF USED, IT IS THE RESPONSIBILITY OF THE MANUFACTURER TO PROVIDE EVIDENCE OF COMPLIANCE TO AS9100. THE QUALIFYING ACTIVITY (QA) AUTHORITY RESERVES THE RIGHT TO MONITOR, MEASURE, AND VALIDATE COMPLIANCE AT
31、 THEIR DISCRETION. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/88SHEET 6 OF 6REV. A(R) CONTACTS, ELECTRICAL CONNECTOR SOCKET, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL
32、-38999 SERIES I, III, IV CONNECTORS) APPLICATION NOTES: 1. CONTACT MATES DIRECTLY TO AN AS39029/87 PIN AS SHOWN IN TABLE 6. TABLE 6 - CONTACT MATING PART NUMBERS AS39029/88 BIN CODE MATING AS39029/87 SLASH SHEET/BIN CODE -482 -470-483 -471 -484 -472-485 -473-486 -474-487 -475-488 -476-489 -477-490 -
33、478 -491 -479-492 -480-493 -4812. THE COMPOSITION DESIGNATIONS HAVE BEEN CHANGED AS LISTED BELOW: JN = TYPE J NEGATIVE (FORMERLY CONSTANTAN) KN = TYPE K NEGATIVE (FORMERLY ALUMEL) KP = TYPE K POSITIVE (FORMERLY CHROMEL) JP = TYPE J POSITIVE (FORMERLY IRON) 1. SPECIFICATION NOTES: NOTICE THIS DOCUMEN
34、T REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. 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 T
35、O 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-,-,-
