1、 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 particular use, including any patent infringement arising there
2、from, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2012 SAE International All rights reserved. No part of this publication m
3、ay 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: +1 724-776-4970 (outside U
4、SA) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.org SAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/AMS5853C AEROSPACE MATERIAL SPECIFICATION AMS5853 REV. C Issued 1987-10 Revised 2006-06 Reaff
5、irmed 2012-04 Superseding AMS5853B Steel, Corrosion and Heat-Resistant, Bars and Wire 15Cr - 25.5Ni - 1.2Mo - 2.1Ti - 0.006B - 0.30V Consumable Electrode Melted 1800 F (982 C) Solution Treated and Work-Strengthened 160 ksi (1103 MPa) Tensile Strength (Composition similar to UNS S66286) RATIONALE AMS5853C has been reaffirmed to comply with the SAE five-year review policy. SAE AMS5853C Page 2 of 5 SAE AMS5853C Page 3 of 5 SAE AMS5853C Page 4 of 5 SAE AMS5853C Page 5 of 5
