SAE-AS-39029-98-2000-R2006.pdf

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SHEET 1 OF 4 AS39029/98 THIRD ANGLE PROJECTION AEROSPACE STANDARD AS39029/98 ISSUED 2000-07 CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 1 (FOR DOD-C-83527 CONNECTORS) PREPARED BY SAE SUBCOMMITTEE AE-8C1 FEDERAL SUPPLY CLASS 5935 NOTICE THIS DOCUMENT HAS BEEN TAKEN DIRECTLY FROM U.S. MILITARY SPECIFICATION MIL-C-39029/98A AND 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 UNCHANGED. 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 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 LISTS 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. RATIONALE THIS DOCUMENT HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE 5-YEAR REVIEW POLICY. REAFFIRMED 2006-08 Copyright 2006 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, 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: 724-776-4970 (outside USA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org Copyright SAE International Provided by IHS under license with SAELicensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 09/10/2007 03:17:10 MDTNo reproduction or networking permitted without license from IHS -,-,- CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 1 (FOR DOD-C-83527 CONNECTORS) AEROSPACE STANDARD AS39029/98 SHEET 2 OF 4 AS39029/98 THE REQUIREMENTS FOR ACQUIRING THE CONTACTS DESCRIBED HEREIN SHALL CONSIST OF THIS SPECIFICATION AND THE LATEST ISSUE OF MIL-C-39029. FIGURE 1. SOCKET CONTACTS. Copyright SAE International Provided by IHS under license with SAELicensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 09/10/2007 03:17:10 MDTNo reproduction or networking permitted without license from IHS -,-,- CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 1 (FOR DOD-C-83527 CONNECTORS) AEROSPACE STANDARD AS39029/98 SHEET 3 OF 4 AS39029/98 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 rubber. Plating: Gold as required for MIL-C-39029, type D contacts. Performance: Temperature range: -65°C to +165°C. 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. Rated voltage: 1,000 V rms at sea level. Copyright SAE International Provided by IHS under license with SAELicensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 09/10/2007 03:17:10 MDTNo reproduction or networking permitted without license from IHS -,-,- CONTACTS, ELECTRICAL CONNECTOR, SOCKET, CRIMP REMOVABLE, COAXIAL, SIZE 1 (FOR DOD-C-83527 CONNECTORS) AEROSPACE STANDARD AS39029/98 SHEET 4 OF 4 AS39029/98 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-1344. Directions shall be longitudinal and perpendicular. 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 unassembled in a suitable container. Manufacturer recommended 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 SAELicensee=IHS Employees/1111111001, User=Wing, Bernie Not for Resale, 09/10/2007 03:17:10 MDTNo reproduction or networking permitted without license from IHS -,-,-