1、 AEROSPACE STANDARD TERMINAL JUNCTION SYSTEM, GROUNDED STUD, SERIES I AS81714/15Copyright 2012 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, recordi
2、ng, 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 ISSUED 2000-03REAFFIRMED 2012-01THIRD ANGLE PROJEC
3、TION CUSTODIAN: AE-8C2 FEDERAL SUPPLY CLASS 5940 AS81714/15SHEET 1 OF 3 SAE Technical Standards Board Rules provide that: “This report ispublishedby SAE toadvance thestate of technicalandengineering sciences. Theuse ofthis report is entirely voluntary, andits applicability and suitability forany par
4、ticular 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. SAE invites yourwrittencomments andsuggestions. SAE values your input. To
5、 provide feedbackon this Technical Report, please visit http:/www.sae.org/technical/standards/AS81714/15 RATIONALE AS81714/15 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. NOTICETHIS DOCUMENT HAS BEEN TAKEN DIRECTLY FROM U.S. MILITARY SPECIFICATION MIL-T-81714/15C AND CONTAINS
6、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-T-81714/15C. ANY PART NUMBERS ESTABLISHED BY THE ORIGINAL SPECIFICATION REMAIN UNCHANGED.THE ORIG
7、INAL 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
8、 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 MA
9、NDATORY 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.AEROSPACE STANDARD AS81714/15SHEET 2 OF 3 TERMINAL JUNCTION SYSTEM, GROUNDED STUD, SERIES I THE COMPLETE REQUIREMENTS FOR ACQUIRING THE WI
10、RE IN-LINE JUNCTION DESCRIBED HEREIN SHALL CONSIST OF THIS DOCUMENT AND THE LATEST ISSUE OF SPECIFICATION MIL-T-81714.TABLE I. TERMINALS.AEROSPACE STANDARD AS81714/15SHEET 3 OF 3 TERMINAL JUNCTION SYSTEM, GROUNDED STUD, SERIES I REQUIREMENTS:1. STUD, HEX AND SHOULDER: THE STUD, HEX AND SHOULDER SHAL
11、L BE COPPER ALLOY AND SHALL BE GOLDPLATED IN ACCORDANCE WITH MIL-G-45204, TYPE I, GRADE C, CLASS 00 OVER A SUITABLE NICKELUNDERPLATE.2. TOOL FOR CONTACT INSERTING/REMOVAL SHALL BE ORDERED SEPARATELY (SEE TABLE I).NOTES:1. DIMENSIONS ARE IN INCHES.2. METRIC EQUIVALENTS (TO THE NEAREST .01 MM) ARE GIV
12、EN FOR GENERAL INFORMATION ONLY AND AREBASED UPON 1 INCH = 25.4 MM.3. INTERNATIONAL INTEREST, SEE SPECIFICATION MIL-T-81714.4. THE PART NUMBER CONSISTS OF THE LETTER M, SPECIFICATION SHEET NUMBER, COMPONENTDESIGNATOR, AND CLASS.PART NUMBER EXAMPLE:M81714/15-20DSIZE 20 TERMINAL.5. CLASSES A, B AND C COMPONENTS ARE INACTIVE FOR NEW DESIGN. ONLY CLASS D COMPONENTS SHALLBE USED FOR DIRECT GOVERNMENT ACQUISITION.
