SAE AMS 3898 6A-1994 Interleaf Carrier Material Composite Tape Differentially Coated Paper Unperforated 0 0035 inch (0 081 mm)《未穿孔0 0032 in(0 081 mm)复合胶带差异涂覆纸中间层载体材料》.pdf

《SAE AMS 3898 6A-1994 Interleaf Carrier Material Composite Tape Differentially Coated Paper Unperforated 0 0035 inch (0 081 mm)《未穿孔0 0032 in(0 081 mm)复合胶带差异涂覆纸中间层载体材料》.pdf》由会员分享，可在线阅读，更多相关《SAE AMS 3898 6A-1994 Interleaf Carrier Material Composite Tape Differentially Coated Paper Unperforated 0 0035 inch (0 081 mm)《未穿孔0 0032 in(0 081 mm)复合胶带差异涂覆纸中间层载体材料》.pdf（2页珍藏版）》请在麦多课文档分享上搜索。

1、1. SCOPE:1.1 Form:This specification covers a paper, coated on both sides and with differentrelease characteristics on each side (i.e., differentially coated), suppliedin the form of rolls of sheeting or reels of unperforated tape of the widthspecified.2. APPLICABLE DOCUMENTS:See AMS 3898.3. TECHNIC

2、AL REQUIREMENTS:3.1 Basic Specification:The complete requirements for procuring the product described herein shallconsist of this document and the latest issue of the basic specification,AMS 3898.3.2 Material:(R)The carrier material shall be a paper with a heat-cured silicone emulsioncoating on each

3、 side. The coating on one side shall provide a controlledrelease from composite prepreg materials while the other side shall providean easy release from these same composite prepreg materials, with no transferof coating to the composite prepreg surface.3.2.1 Thickness: Shall be 0.0032 inch 0.0005 (0

4、.081 mm 0.012).3.2.2 Width: Shall be as ordered.AEROSPACE MATERIAL SPECIFICATIONAMS3898/6 REV. A Issued 1984-04Revised 1994-02Reaffirmed 2014-08Superseding AMS3898/6Interleaf Carrier Material, Composite TapeDifferentially Coated Paper, Unperforated0.0035 inch (0.081 mm)RATIONALEAMS3898/6A has been r

5、eaffirmed to comply with the SAE five year review policy._SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particu

6、lar use, including any patent infringement arising therefrom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2014 SA

7、E InternationalAll 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.877-606-7323 (inside USA and Canada)

8、TO PLACE A DOCUMENT ORDER: Tel: Tel: +1 724-776-4970 (outside USA)SAE WEB ADDRESS:Fax: 724-776-0790Email: CustomerServicesae.orghttp:/www.sae.orgSAE values your input. To provide feedbackon this Technical Report, please visithttp:/www.sae.org/technical/standards/AMS3898/6ASAE INTERNATIONAL AMS3898/6

9、A Page 2 of 2 3.3 Properties:Shall be as shown in Table 1.TABLE 1 - Propertiesraph Paragraph Requirement Test Method3.3.1 Tensile Strength, minimum 15 pounds forceper inch(2.63 kN/m) of widthASTM D 882,Method A3.3.2 Tear Strength, minimum 1.6 ounces force(445 mN)ASTM D 827-714. QUALITY ASSURANCE PROVISIONS:See AMS 3898.5. PREPARATION FOR DELIVERY:See AMS 3898.6. ACKNOWLEDGMENT:See AMS 3898.7. REJECTIONS:See AMS 3898.8. NOTES:See AMS 3898.