1、AEROSPACE STANDARD (R) CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL-38999 SERIES I, II, III, AND IV, MIL-DTL-24308, AND MIL-DTL-83733) AS39029/87Copyright 2009 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retriev
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3、vicesae.org SAE WEB ADDRESS: http:/www.sae.org ISSUED 2000-07 REVISED 2009-09 THIRD ANGLE PROJECTION CUSTODIAN: AE-8C1 REV.AFEDERAL SUPPLY CLASS 5999 AS39029/87SHEET 1 OF 6REV. APROCUREMENT SPECIFICATION: AS39029SAE TechnicalStandards Board Rules provide that: “This report is published by SAE toadva
4、nce thestate of technical andengineering sciences. Theuse of thisreport is entirely voluntary, andits applicabilityandsuitability forany particularuse, including any patent infringement arising therefrom, is thesole responsibility oftheuser.”SAE reviews each technical report at least every five year
5、sat which time it may be reaffirmed, revised, orcancelled. SAE invites yourwritten commentsandsuggestions. SAE VALUES YOUR INPUT. TO PROVIDE FEEDBACK ON THIS TECHNICAL REPORT, PLEASE VISIT http:/www.sae.org/technical/standards/AS39029/87ARATIONALE REVISE TO INCLUDE COMMENTS RECEIVED BY THE GOVERNMEN
6、T AND INDUSTRY, 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 AS3902
7、9.FIGURE 1 - PIN CONTACTS Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/87SHEET 2 OF 6REV. A(R) CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, THERMOCOUPLE (FOR MI
8、L-DTL-38999 SERIES I, II, III, AND IV, MIL-DTL-24308, AND MIL-DTL-83733) TABLE 1 - CONTACT DIMENSIONS BIN CODEARADIUSB DIA C DIA D DIA E DIA F DIA G DIA H K M470 THRU 473.020 (.51) .010 (.25).0305 (.77) .0295 (.75).062 (1.57) .060 (1.52).022 (.56).018 (.46).0355 (.90) .0335 (.85).011(.28)MAX.048(1.2
9、2).046(1.17).005(.13).003(.08).157 (3.99) .141 (3.58)N/A474 THRU 477.020 (.51) .015 (.38).041 (1.04).039 (.99).094 (2.39) .091 (2.31).032 (.81).026 (.66).048 (1.22).046 (1.17).015(.38)MAX.070(1.78).068(1.73).078(1.98).072(1.83)478 THRU 481.025 (.64) .020 (.51).0635(1.61).0615(1.56).130 (3.30) .127 (
10、3.23).042 (1.07) .036 (.91).068 (1.73).066 (1.68).030(.76).011(.28).103(2.62).101(2.57).088(2.24).082(2.08).010(.25).005(.13).229 (5.82) .209 (5.31)TABLE 2 - MARKING AND DESIGN CHARACTERISTICS BINCODE COLOR BANDS MATING END SIZEWIREBARRELLSIZETYPE CLASS 1ST2ND3RD470 YELLOW VIOLET BLACK 22 22D C B 47
11、1 YELLOW VIOLET BROWN 22 22D 472 YELLOW VIOLET RED 22 22D 473 YELLOW VIOLET ORANGE 22 22D 474 YELLOW VOILET YELLOW 20 20 475 YELLOW VIOLET GREEN 20 20 476 YELLOW VIOLET BLUE 20 20 477 YELLOW VIOLET VIOLET 20 20 478 YELLOW VIOLET GRAY 16 16 479 YELLOW VIOLET WHITE 16 16 480 YELLOW GRAY BLACK 16 16 48
12、1 YELLOW GRAY BROWN 16 16 Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/87SHEET 3 OF 6REV. A(R) CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, THERMOCOUPLE (FOR MI
13、L-DTL-38999 SERIES I, II, III, AND IV, MIL-DTL-24308, AND MIL-DTL-83733) TABLE 3 - TOOLS BIN CODE BASIC CRIMPING TOOL POSITIONER INSTALLING TOOL REMOVAL TOOL 470, 471, 472, 473 M22520/2-01 OR M22520/7-01 M22520/2-09 OR M22520/7-07 M81969/8-01 OR M81969/14-01 M81969/8-02 OR M81969/14-01 474, 475, 476
14、 477 M22520/1-01 OR M22520/2-01 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 M81969/14-02 478, 479, 480, 481 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, PLAT
15、ING, AND TENSILE STRENGTH BIN CODE MATERIALS PLATING TENSILE STRENGTH 1/WIRE SIZE AXIAL LOAD WIRE SIZE AXIAL LOAD 470 JN NONE 28 MIN 1.5 22 MAX 6 471 KN NONE 472 KP NONE 473 JP CADMIUM PLATE 2/474 JN NONE 24 MIN 4.5 20 MAX 14 475 KN NONE 476 KP NONE 477 JP CADMIUM PLATE 2/478 JN NONE 20 MIN 14 16 MA
16、X 33 479 KN NONE 480 KP NONE 481 JP CADMIUM PLATE 2/1/ APPLIES TO TYPE 1 WIRE PER MIL-W-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 AS39029/87SHEET
17、4 OF 6REV. A(R) CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL-38999 SERIES I, II, III, AND IV, MIL-DTL-24308, AND MIL-DTL-83733) TABLE 5 - PART NUMBER AND BIN CODE PART NUMBER BIN CODE SUPERSEDED M39029/87-470 470 M39029/872222C1 M39029/87-471 471 M39029/872222C2 M3
18、9029/87-472 472 M39029/872222C3 M39029/87-473 473 M39029/872222C4 M39029/87-474 474 1/ M39029/872020C1 M39029/87-475 475 1/ M39029/872020C2 M39029/87-476 476 1/ M39029/872020C3 M39029/87-477 477 1/ M39029/872020C4 M39029/87-478 478 1/ M39029/871616C1 M39029/87-479 479 1/ M39029/871616C2 M39029/87-48
19、0 480 1/ M39029/871616C3 M39029/87-481 481 1/ M39029/871616C4 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 AND AS39029/10. REQUIREMENTS: ALL REQUIREMENTS SHALL CONSIST OF THIS SPECIFICATION AND THE LATEST ISSUE OF AS39029. 1.
20、 DESIGN; CONTACTS SHALL BE DESIGNED IN ACCORDANCE WITH FIGURE 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 FEATUR
21、E SIZE (RFS); FOR ALL OTHER CONTACT SIZES, DIAMETERS E AND G TO BE CONCENTRIC WITHIN .001 (TIR) AT MAXIMUM MATERIAL CONDITION (MMC). SPHERICAL END DIMENSIONS SHALL CONFORM TO AS39029/58. 2. TOOLS: TOOLS REQUIRED FOR CRIMPING CONTACTS TO THE WIRE/CABLE AND THE INSTALLING/REMOVAL FROM THE CONNECTOR SH
22、ALL BE IN ACCORDANCE WITH TABLE 3. 3. PART NUMBERS: CONTACT PART NUMBERS SHALL BE IN ACCORDANCE WITH TABLE 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 WIT
23、H EIA-364-28 THE FOLLOWING DETAILS SHALL APPLY: a. TEST CONDITION V USING THE VIBRATION ENVELOPE SHOWN IN FIGURE 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 DIREC
24、TION AND 8 HOURS IN A PERPENDICULAR DIRECTION FOR A TOTAL OF 16 HOURS. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/87SHEET 5 OF 6REV. A(R) CONTACTS, ELECTRICAL CONNECTO
25、R, PIN, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL-38999 SERIES I, II, III, AND IV, MIL-DTL-24308, AND MIL-DTL-83733) FIGURE 2 - VIBRATION 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 MILLIAMP
26、ERES MAXIMUM CURRENT FLOW THROUGH THE SERIES CIRCUIT DURING HIGH-IMPACT SHOCK. CONNECTORS SHALL BE MONITORED FOR ANY DISCONTINUITIES. A DETECTOR 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 M
27、IL-S-901, GRADE A WITH THE FOLLOWING MODIFICATIONS AND ADDITIONS. MOUNTING FIXTURE SHALL BE IN ACCORDANCE WITH MIL-S-901, LIGHT WEIGHT. THE 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
28、 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 BE PROVIDED WITH STRAIGHT, OPEN FRAME, STRAIN RELIEF ACCESSORY HARDWARE. 8. QUALIFICATION: THE MANUFACTURERS RELIABILITY ASSURANCE PROGRAM SHALL COMPLY WITH THE AS9
29、100 AEROSPACE STANDARD FOR QUALITY MANAGEMENT SYSTEM REQUIREMENTS. OTHER ESTABLISHED AND INDUSTRY RECOGNIZED QUALITY ASSURANCE STANDARDS THAT ASSURE ALL PRODUCTS PRODUCED CONFORM TO THE CONTRACT REQUIREMENTS ARE ACCEPTABLE. HOWEVER, IF USED, IT IS THE RESPONSIBILITY OF THE MANUFACTURER TO PROVIDE EV
30、IDENCE OF COMPLIANCE TO AS9100. THE QUALIFYING ACTIVITY (QA) AUTHORITY RESERVES THE RIGHT TO MONITOR, MEASURE, AND VALIDATE COMPLIANCE AT THEIR DISCRETION. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS
31、AEROSPACE STANDARD AS39029/87SHEET 6 OF 6REV. A(R) CONTACTS, ELECTRICAL CONNECTOR, PIN, CRIMP REMOVABLE, THERMOCOUPLE (FOR MIL-DTL-38999 SERIES I, II, III, AND IV, MIL-DTL-24308, AND MIL-DTL-83733) APPLICATION NOTES: 1. CONTACT MATES DIRECTLY TO AS39029/88 AND AS39029/89 AS SHOWN IN TABLE 6. TA
32、BLE 6 - CONTACT MATING PART NUMBERS AS39029/87 BIN CODE MATING AS39029 SLASH SHEET/BIN CODE -470 M39029/88-482, M39029/89-494-471 M39029/88-483, M39029/89-495-472 M39029/88-484, M39029/89-496-473 M39029/88-485, M39029/89-497-474 M39029/88-486, M39029/89-498-475 M39029/88-487, M39029/89-499 -476 M390
33、29/88-488, M39029/89-500-477 M39029/88-489, M39029/89-501-478 M39029/88-490, M39029/89-502-479 M39029/88-491, M39029/89-503-480 M39029/88-492, M39029/89-504-481 M39029/88-493, M39029/89-505 2. THE COMPOSITION DESIGNATIONS HAVE BEEN CHANGED AS LISTED BELOW: JN = TYPE J NEGATIVE (FORMERLY CONSTANTAN)
34、KN = TYPE K NEGATIVE (FORMERLY ALUMEL) KP = TYPE K POSITIVE (FORMERLY CHROMEL) JP = TYPE J POSITIVE (FORMERLY IRON) 1. SPECIFICATION NOTES: NOTICE THIS DOCUMENT REFERENCES A PART WHICH CONTAINS CADMIUM AS A PLATING MATERIAL. CONSULT LOCAL OFFICIALS IF YOU HAVE QUESTIONS CONCERNING CADMIUMS USE. A CH
35、ANGE 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 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-,-,-
