SAE AS 39029 98A-2013 CONTACTS ELECTRICAL CONNECTOR SOCKET CRIMP REMOVABLE COAXIAL SIZE 1 (FOR DOD-C-83527 CONNECTORS)《接触点 插座 折边可移动的共轴的电气连接件(DOD-C-83527连接件用)》.pdf

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1、AEROSPACE STANDARD CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 1 (FOR DOD-C-83527 CONNECTORS) AS39029/98Copyright 2013 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 m

2、eans, electronic, 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

3、 ISSUED 2000-07REAFFIRMED 2006-08 STABILIZED 2013-12 THIRD ANGLE PROJECTION CUSTODIAN: AE-8/AE-8C1 REV.AFEDERAL SUPPLY CLASS 5935 AS39029/98REV. ASAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse ofthis rep

4、ort 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 berevised, reaffirmed, stabilized, orcancelled.

5、 SAE invites yourwrittencomments andsuggestions. SAE values your input. To provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS39029/98ARATIONALE THE C1 COMMITTEE HAS RECOMMENDED STABILIZATION OF THIS DOCUMENT BASED ON NO QPL SOURCES AND NO KNOWN USAGE. ANY

6、 EDITORIAL OR TECHNICAL CHANGES NEEDED TO ALIGN THIS DOCUMENT WITH SIMILAR CURRENTLY PUBLISHED DETAIL SHEETS SHALL BE MADE AT SUCH TIME A POTENTIAL SOURCE REQUESTS AUTHORIZATION TO QUALIFY TO THIS DOCUMENT. STABILIZED NOTICE THIS DOCUMENT HAS BEEN DECLARED “STABILIZED“ BY THE SAE AE-8C1 CONNECTORS C

7、OMMITTEE AND WILL NO LONGER BE SUBJECTED TO PERIODIC REVIEWS FOR CURRENCY. USERS ARE RESPONSIBLE FOR VERIFYING REFERENCES AND CONTINUED SUITABILITY OF TECHNICAL REQUIREMENTS. NEWER TECHNOLOGY MAY EXIST. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction o

8、r networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/98 SHEET 1 OF 4 REV. A CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 1 (FOR DOD-C-83527 CONNECTORS) NOTICETHIS DOCUMENT HAS BEEN TAKEN DIRECTLY FROM U.S. MILITARY SPECIFICATION MIL-C-39029/98A AND

9、 CONTAINS ONLY MINOR EDITORIAL AND FORMAT CHANGES REQUIRED TO BRING IT INTO CONFORMANCE WITH THE PUBLISHING REQUIREMENTS OF SAE TECHNICAL STANDARDS. THE INITIAL RELEASE OF THIS DOCUMENT IS INTENDED TO REPLACE MIL-C-39029/98A. ANY PART NUMBERS ESTABLISHED BY THE ORIGINAL SPECIFICATION REMAIN UNCHANGE

10、D.THE ORIGINAL MILITARY SPECIFICATION WAS ADOPTED AS AN SAE STANDARD UNDER THE PROVISIONS OF THE SAE TECHNICAL STANDARDS BOARD (TSB) RULES AND REGULATIONS (TSB 001) PERTAINING TO ACCELERATED ADOPTION OF GOVERNMENT SPECIFICATIONS AND STANDARDS. TSB RULES PROVIDE FOR (A) THE PUBLICATION OF PORTIONS OF

11、 UNREVISED GOVERNMENT SPECIFICATIONS AND STANDARDS WITHOUT CONSENSUS VOTING AT THE SAE COMMITTEE LEVEL, AND (B) THE USE OF THE EXISTING GOVERNMENT SPECIFICATION OR STANDARD FORMAT.UNDER DEPARTMENT OF DEFENSE POLICIES AND PROCEDURES, ANY QUALIFICATION REQUIREMENTS AND ASSOCIATED QUALIFIED PRODUCTS LI

12、STS ARE MANDATORY FOR DOD CONTRACTS. ANY REQUIREMENT RELATING TO QUALIFIED PRODUCTS LISTS (QPLS) HAS NOT BEEN ADOPTED BY SAE AND IS NOT PART OF THIS SAE TECHNICAL DOCUMENT.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without

13、license from IHS-,-,-AEROSPACE STANDARD AS39029/98 SHEET 2 OF 4 REV. A CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 1 (FOR DOD-C-83527 CONNECTORS) THE REQUIREMENTS FOR ACQUIRING THE CONTACTS DESCRIBED HEREIN SHALL CONSIST OF THIS SPECIFICATION AND THE LATEST ISSUE OF MIL-C-

14、39029.FIGURE 1. SOCKET CONTACTS.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/98 SHEET 3 OF 4 REV. A CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZ

15、E 1 (FOR DOD-C-83527 CONNECTORS) FIGURE 1. SOCKET CONTACTS - CONTINUED.REQUIREMENTS:Dimensions and configuration: See figure 1 and table I.Mating contact: MIL-C-39029/97A.Materials:Body: Brass, half-hard or copper-beryllium.Insulator: MIL-P-19468.Crimp ferrule: Copper, annealed.Gasket: Silicone rubb

16、er.Plating: Gold as required for MIL-C-39029, type D contacts.Performance:Temperature range: -65C to +165C.Impedance: 50 ohms nominal.VSWR: 1.70:1 maximum.Frequency range: 0 to 5 GHz.Insertion loss: 0.3 dB.Contact resistance:Outer contact: 0.2 milliohm maximum.Inner contact: 1.0 milliohm maximum.Rat

17、ed voltage: 1,000 V rms at sea level.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-AEROSPACE STANDARD AS39029/98 SHEET 4 OF 4 REV. A CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL

18、 SIZE 1 (FOR DOD-C-83527 CONNECTORS) Dielectric withstanding voltage: 2,500 V rms at sea level.Insulation resistance: 5,000 megohms minimum.Cable retention: 125 pounds minimum.Shock: Test condition D per method 2004 of MIL-STD-1344.Vibration: Test condition VI, letter J, per method 2005 of MIL-STD-

19、1344. Directions shall be longitudinal andperpendicular. Time duration shall be 8 hours in each direction.Installation and removal: Installation and removal of contact shall be per manufacturer recommended instructions.Shipping: Figure 1 illustrates final assembly; parts are to be shipped unassemble

20、d in a suitable container. Manufacturerrecommended assembly instructions shall be shipped with each unit package.QPL evaluating activity: Defense Electronics Supply Center (DESC-E), Dayton, OH 45444.Part number: M39029/98-548.TABLE I. DESIGN CHARACTERISTICS.Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

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