1、 AEROSPACE STANDARD CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 12 (FOR MIL-DTL-38999 SERIES I, III AND IV CONNECTORS) AS39029/103 Copyright 2017 SAE International All rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitt
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3、 ADDRESS: http:/www.sae.org ISSUED2000-09REVISED 2017-09THIRD ANGLE PROJECTION CUSTODIAN: AE-8/AE-8C1 REV.B FEDERAL SUPPLY CLASS 5999 AS39029 /103 SHEET 1 OF 6 REV. B PROCUREMENT SPECIFICATION: AS39029 SAE Technical Standards Board Rules provide that: “This report is published by SAEtoadvance thesta
4、te of technicaland engineering sciences. The useof this report is entirely voluntary, and its applicability andsuitability for any particularuse, includingany patent infringement arisingtherefrom,is thesole responsibility of theuser.” SAE reviews eachtechnical reportatleast every fiveyears at whicht
5、ime it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.SAE values your input. To provide feedback on this Technical Report, please visit http:/standards.sae.org/AS39029/103B RATIONALE REVISION IS REQUIRED TO CORRECT THE DOCUMENT TITLE TO INDICA
6、TE IT IS A SOCKET RATHER THAN A PIN, AND ALSO CORRECT THE CONNECTOR APPLICATIONS TO MIL-DTL-38999 SERIES 1, III AND IV. NOTICE THE COMPLETE REQUIREMENTS FOR PROCURING THE PRODUCT DESCRIBED HEREIN SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF AS39029. FIGURE 1 - SOCKET CONTACTS AEROSPACE STA
7、NDARD AS39019 /103 SHEET 2 OF 6 REV. B CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 12 (FOR MIL-DTL-38999 SERIES I, III AND IV CONNECTORS) TABLE 1 - DIMENSIONS BIN CODE A DIA C DIA D DIA E DIA F DIA G DIA MAX H DIA MIN J DIA MAX K L DIA MIN N P V X Z DIA MAX 559 .160 (4.06)
8、 .158 (4.01 .123 (3.12) .118 (3.00) .069 (1.75) .066 (1.68) .151 (3.84) .148 (3.76) .182 (4.62) .179 (4.55) .156 (3.96) .127 (3.23) .169 (4.29) .180 (4.57) .170 (4.32) .022 (.559) .084 (2.13) .100 (2.54) .063 (1.60) .088 (2.24) .0205 (.521) .0195 (.495) .613 (15.57) .603 (15.32) .110 (2.79) TABLE 2
9、 DESIGN CHARACTERISTICS BIN CODE COLOR BANDS CONTACT CAVITY SIZE CABLE ACCOMMODATED. TYPE CLASS 1ST 2ND 3RD 559 GREEN GREEN WHITE 12 M17/113-RG316 M17/094-RG179 D B TABLE 3 TOOLS BIN CODE INNER CONTACT TOOLING 1/ OUTER CONTACT TOOLING INSTALLING TOOL REMOVAL TOOL BASIC CRIMP TOOL/CONTACT POSITIONER
10、 COMBINATIONS BASIC CRIMPING TOOL DIE 559 DEUTSCH-BASIC TOOL - MH992, POSITIONER - KI304 2/ M22520/5-01 M22520/5-03 M81969/8-09 OR M81969/14-04 M81969/8-10 OR M81969/14-04 TRI-STAR-BASIC TOOL - M22520/2-01, POSITIONER - K1457 2/ AMPHENOL-BASIC TOOL - MH992, POSITIONER - K1360 2/ 1/ INNER CONTACT MAY
11、 BE CRIMPED OR SOLDERED. 2/ SEE REQUIREMENT NOTE 8 AND APPLICATION NOTE 3. TABLE 4 - CONTACT RESISTANCE BIN CODE CABLE ACCOMMODATED MAXIMUM VOLTAGE DROP (MILLIVOLTS) MAXIMUM AVERAGE VOLTAGE DROP 25 C +3, -0 25 C +3, -0 1/ 200 C +3, -0 INNER OUTER INNER OUTER INNER OUTER 559 M17/094-RG179 M17/113-RG3
12、16 55 120 75 70 66 144 90 84 94 204 128 119 N/A N/A 1/ AFTER CONDITIONING TABLE 5 - LOW SIGNAL LEVEL CONTACT RESISTANCE (INNER CONTACT ONLY) AND TENSILE STRENGTH BIN CODE CABLE ACCOMMODATED MAXIMUM CONTACT RESISTANCE (MILLIOHMS) TENSILE LOAD (POUNDS MINIMUM) INITIAL AFTER CONDITIONING INNER CONTACT
13、OUTER CONTACT 559 M17/094-RG179 M17/113-RG316 55 120 66 144 10.0 3.5 15.0 15.0 AEROSPACE STANDARD AS39019 /103 SHEET 3 OF 6 REV. B CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 12 (FOR MIL-DTL-38999 SERIES I, III AND IV CONNECTORS) TABLE 6 - CONTACT ENGAGEMENT AND SEPARATION
14、 FORCE TEST PIN DIAMETER (INCH) MINIMUM SEPARATION FORCE (OUNCES) MAXIMUM ENGAGEMENT FORCE (OUNCES) MAXIMUM AVERAGE ENGAGEMENT FORCE INITIAL AFTER CONDITIONING INITIAL AFTER CONDITIONING .0950 (2.41) +.0002 (0.005) -.0000 (0.000) N/A N/A 30 36 N/A .0930 (2.36) +.0000 (0.000) -.0002 (0.005) 3.0 2.5 N
15、/A N/A N/A TABLE 7 - PART NUMBER AND BIN CODE PART NUMBER BIN CODE SUPERSEDED PART NUMBER M39029/103-559 559 N/A REQUIREMENTS: 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. DIMENSION
16、S SHOWN APPLY AFTER PLATING. 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 INNER CONTACT SPRING. PROVISION FOR CLEARANCE HOLE SHALL BE PROVIDED. CRIMP DEFORMATION: THE MAXIMUM DIAMETER OVER THE CRIMPED PORTION OF TH
17、E SHIELD CRIMP SLEEVE SHALL NOT EXCEED G DIAMETER. 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 7. SUPERSEDED PART NUMBERS AR
18、E AS SPECIFIED. 4. MATERIALS: MATERIALS SHALL BE IN ACCORDANCE WITH AS39029. 5. MECHANICAL: MECHANICAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS39029. CONTACT ENGAGEMENT AND SEPARATION FORCES (INNER SOCKET CONTACT ONLY): THE ENGAGEMENT DEPTH SHALL BE AS ENCOUNTERED IN NORMAL SERVICE. THE TEST PINS S
19、HALL BE IN ACCORDANCE WITH AS31971 EXCEPT THE DIAMETERS SHALL BE AS SPECIFIED IN TABLE 6, AND SURFACE ROUGHNESS SHALL NOT EXCEED 3 MICROINCHES. PROVISION FOR CLEARANCE HOLE SHALL BE PROVIDED. TENSILE STRENGTH (INNER AND OUTER CONTACT): SEE TABLE 5. 6. ELECTRICAL: ELECTRICAL PROPERTIES SHALL BE IN AC
20、CORDANCE WITH AS39029. CONTACT RESISTANCE: SEE TABLE 4. TEST CURRENT: INNER CONTACT - 1.0 AMPERE. OUTER CONTACT - 12.0 AMPERES. AEROSPACE STANDARD AS39019 /103 SHEET 4 OF 6 REV. B CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 12 (FOR MIL-DTL-38999 SERIES I, III AND IV CONNEC
21、TORS) LOW SIGNAL LEVEL CONTACT RESISTANCE (INNER CONTACT ONLY): SEE TABLE 5. NOMINAL IMPEDANCE: 50 OHMS. VOLTAGE STANDING WAVE RATIO (VSWR) (APPLICABLE TO M17/113-RG316 CABLE ONLY): a. THE VSWR OF THIS PIN CONTACT MATED WITH A MIL-C-39029/103 SOCKET CONTACT SHALL NOT EXCEED 1.20 .04F (F IN GHz) FROM
22、 500 MHz TO 3 GHz UNDER ALL OF THE FOLLOWING CONDITIONS. THESE CONDITIONS APPLY WHEN THE CONTACTS ARE ASSEMBLED TO M17/113-RG316 CABLES: 1. PIN AND SOCKET CONTACTS ENGAGED, .755 .005 FROM RETENTION SHOULDER TO RETENTION SHOULDER. 2. PIN AND SOCKET CONTACTS ENGAGED, .783 .005 FROM RETENTION SHOULDER
23、TO RETENTION SHOULDER. 3. PIN AND SOCKET CONTACTS ENGAGED, .810 .005 FROM RETENTION SHOULDER TO RETENTION SHOULDER. b. SWEPT FREQUENCY VSWR TEST SETUP: MATED PAIR OF CONTACTS SHALL BE TESTED USING A HEWLETT-PACKARD 8510 VECTOR NETWORK ANALYZER AS FOLLOWS: 1. USE THE HEWLETT-PACKARD 8510 CALIBRATED A
24、T THE OUTPUT PORT OR AT A CONNECTOR SAVER CONNECTED TO THE OUTPUT PORT. 2. SWEEP-RAMP MODE, 401 POINTS, 500 MHz TO 3.0 GHz. 3. MAKE UP ONE RG316 CABLE ASSEMBLY (APPROXIMATELY 6 INCHES LONG) WITH A MIL-C-39029/102 ON ONE END AND AN SMA CONNECTOR ON THE OTHER END. 4. MAKE UP ANOTHER RG316 CABLE ASSEMB
25、LY (APPROXIMATELY ONE FOOT LONG) WITH A MIL-C-39029/103 ON ONE END AND AN SMA CONNECTOR ON THE OTHER END. 5. TERMINATE THE SMA CONNECTOR ON THE LONGER ASSEMBLY WITH A 50 OHM LOAD AND MATE PER ENGAGEMENT POSITION 1 THE MIL-C-39029/102 AND MIL-C-39029/103 CONTACTS. 6. CONNECT THE OTHER SMA CONNECTOR T
26、O THE APC-3.5 PORT WHICH HAD BEEN CALIBRATED. 7. CHANGE THE DISPLAY TO TIME DOMAIN, BAND PASS. 8. SET THE GATE CENTER AT THE COAXIAL CONTACT INTERFACE AND THE GATE WIDTH AT 2.25 NANOSECONDS. 9. TURN THE GATE ON AND RETURN TO THE FREQUENCY DOMAIN. 10. PLOT THE CONNECTOR PAIR VSWR (S11). 11. VERIFY TH
27、AT THE DISPLAYED VSWR (S11) COMPLIES WITH THE VSWR LIMITS SPECIFIED FOR THE MATED PAIR OF CONTACTS. 12. REPEAT (5) THROUGH (11) WITH PIN AND SOCKET CONTACTS MATED PER ENGAGEMENT POSITIONS 2 AND 3. INSERTION LOSS (APPLICABLE TO M17/113-RG316 CABLE ONLY): dB MAXIMUM = .11 X F (F IN GHz). WHEN MEASURED
28、 IN ACCORDANCE WITH MIL-C-39012 AT 3 GHz, THE INSERTION LOS SHALL NOT EXCEED .20 dB. DIELECTRIC WITHSTANDING VOLTAGE (APPLIED BETWEEN INNER AND OUTER CONTACT): TEST VOLTAGE: AT SEA LEVEL - 1000 V RMS AT 50000 FEET - 250 V RMS 7. ENVIRONMENTAL: ENVIRONMENTAL PROPERTIES SHALL BE IN ACCORDANCE WITH AS3
29、9029. VIBRATION: TEST CONDITION D, IN ACCORDANCE WITH METHOD 204 OF MIL-STD-202. EXCEPT THE VIBRATION FREQUENCY SHALL BE SINUSOIDAL. AEROSPACE STANDARD AS39019 /103 SHEET 5 OF 6 REV. B CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 12 (FOR MIL-DTL-38999 SERIES I, III AND IV C
30、ONNECTORS) RANDOM VIBRATION: CONNECTORS/CONTACTS SHALL BE TESTED IN ACCORDANCE WITH EIA-364-28, TEST CONDITION V. THE FOLLOWING DETAILS SHALL APPLY: a. USE THE VIBRATION ENVELOPE SHOWN ON FIGURE 2 HEREIN. b. VIBRATION TO BE CONDUCTED AT STANDARD TEST CONDITIONS. c. DURATION SHALL BE 8 HOURS IN THE L
31、ONGITUDINAL AND 8 HOURS IN THE PERPENDICULAR DIRECTION FOR A TOTAL OF 16 HOURS. HIGH IMPACT SHOCK: ALL CONTACTS SHALL BE WIRED IN A SERIES CIRCUIT WITH 100 MILLIAMPERES MAXIMUM CURRENT FLOW THROUGH THE SERIES CIRCUIT DURING SHOCK. CONTACTS SHALL BE MONITORED FOR ANY DISCONTINUITIES. A DETECTOR CAPAB
32、LE OF DETECTING ALL DISCONTINUITIES IN EXCESS OF 1 MICROSECOND SHALL BE USED. WIRED AND MATED CONTACTS SHALL BE SUBJECTED TO THE TEST SPECIFIED IN MIL-C-901, GRADE A WITH THE FOLLOWING MODIFICATIONS AND ADDITIONS. MOUNTING FIXTURE SHALL BE IN ACCORDANCE WITH MIL-C- 901, LIGHT WEIGHT. THE CABLE OR WI
33、RE BUNDLE SHALL BE SUPPORTED ON A STATIONARY FRAME TO PROVIDE A FREE FLEXING CABLE LENGTH BETWEEN THE FRAME AND FIXTURE OF NOT LESS THAN 36 INCHES (914.4 MM): a. COUPLING: COUPLED BY NORMAL MOUNTING MEANS. b. TEST CONDITION A: THE WIRE BUNDLES SHALL BE PROVIDED WITH STRAIGHT, OPEN FRAME, RELIEF ACCE
34、SSORY 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 THAT ASSURE ALL PRODUCTS PRODUCED CONFORM TO THE CONTRAC
35、T 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 THEIR DISCRETION. SHIPPING: FIGURE 1 ILLUSTRATES FINAL
36、ASSEMBLY; PARTS ARE TO BE SHIPPED UNASSEMBLED IN A SUITABLE CONTAINER. MANUFACTURERS RECOMMENDED ASSEMBLY INSTRUCTIONS ARE TO BE SHIPPED WITH THE UNIT PACKAGE. AEROSPACE STANDARD AS39019 /103 SHEET 6 OF 6 REV. B CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 12 (FOR MIL-DTL-3
37、8999 SERIES I, III AND IV CONNECTORS) FIGURE 2 - VIBRATION ENVELOPE APPLICATION NOTES: 1. CONTACT MATES DIRECTLY WITH AN AS39029/103 SOCKET CONTACT AS SHOWN IN TABLE 8. TABLE 8 - CONTACT MATING PART NUMBERS AS39029/103 BIN CODE MATING AS39029 SLASH SHEET/BIN CODE -559 M39029/102-558 2. THIS CONTACT
38、IS NOT RECOMMENDED FOR NEW DESIGN. 3. CONTACT COMPONENT PARTS ARE NOT RECOMMENDED TO BE MIXED BETWEEN QPL SOURCES AND THE CONTACT MANUFACTURERS ASSEMBLY INSTRUCTIONS SHOULD BE STRICTLY FOLLOWED. SPECIFICATION NOTES: 1. REVISION INDICATOR: A CHANGE BAR (l) LOCATED IN THE LEFT MARGIN IS FOR THE CONVEN
39、IENCE 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.
