FORD ESA-M4D434-A1-2010 STYRENE MALEIC ANHYDRIDE TERPOLYMER (SMA) MODIFIED MOLDING COMPOUND GENERAL PURPOSE TO BE USED WITH FORD WSS-M99P1111-A 《通用苯乙烯马来酐三元共聚物(SMA)改性成型料 与标准FORD .pdf
《FORD ESA-M4D434-A1-2010 STYRENE MALEIC ANHYDRIDE TERPOLYMER (SMA) MODIFIED MOLDING COMPOUND GENERAL PURPOSE TO BE USED WITH FORD WSS-M99P1111-A 《通用苯乙烯马来酐三元共聚物(SMA)改性成型料 与标准FORD .pdf》由会员分享,可在线阅读,更多相关《FORD ESA-M4D434-A1-2010 STYRENE MALEIC ANHYDRIDE TERPOLYMER (SMA) MODIFIED MOLDING COMPOUND GENERAL PURPOSE TO BE USED WITH FORD WSS-M99P1111-A 《通用苯乙烯马来酐三元共聚物(SMA)改性成型料 与标准FORD .pdf(3页珍藏版)》请在麦多课文档分享上搜索。
1、 ENGINEERING MATERIAL SPECIFICATION Material Name Specification Number Date Action Revisions 2010 01 07 N-STATUS No replacement named J. Crist, NA 2000 09 25 Revised Updated A. Cockman 1982 09 23 CLN2-1R004101-CL Released R. Ocobock Printed copies are uncontrolled Page 1 of 3 Copyright 2010, Ford Gl
2、obal Technologies, Inc. STYRENE MALEIC ANHYDRIDE TERPOLYMER (SMA), ESA-M4D434-A1 MODIFIED MOLDING COMPOUND, GENERAL PURPOSE NOT TO BE USED FOR NEW DESIGN 1. SCOPE The material defined by this specification is a modified styrene maleic anhydride terpolymer molding compound with high impact strength a
3、nd excellent thermal properties. 2. APPLICATION This specification was released originally for material used in painted wheel cover or ornament applications. 3. REQUIREMENTS Material specification requirements are to be used for initial qualification of materials. 3.1 QUALITY SYSTEM REQUIREMENTS Mat
4、erial suppliers and part producers must conform to the Companys Quality System Requirements. 3.2 INFRARED SPECTROPHOTOMETRY AND/OR THERMAL ANALYSIS IR spectra and thermograms established for initial approval shall constitute the reference standard and shall be kept on file at the designated material
5、 laboratory. All samples shall produce IR spectra and thermograms that correspond to the reference standard when tested under the same conditions. 3.3 CONDITIONING AND TEST CONDITIONS All test values indicated herein are based on material conditioned in a controlled atmosphere of 23 +/- 2 C and 50 +
6、/- 5 % relative humidity for not less than 24 h prior to testing and tested under the same conditions unless otherwise specified. All test values indicated herein are based on material and specimens with moisture content not exceeding 0.3 %. All test materials immediately after processing have to be
7、 sealed in containers that are impermeable to water vapor. If the moisture content exceeds 0.3 %, condition the material for a minimum of 16 h at 40 - 50 C at a reduced pressure below 133 Pa. ENGINEERING MATERIAL SPECIFICATION ESA-M4D434-A1 Page 2 of 3 Copyright 2010, Ford Global Technologies, Inc.
8、Conduct tests in a controlled atmosphere of 23 +/- 2 C and 50 +/- 5 % relative humidity. Individual specimens shall not be removed from closed containers until immediately before testing. 3.4 MOLDED TEST SPECIMENS 3.4.1 Specific Gravity, min 1.04 (ASTM D 792) 3.4.2 Tensile Strength, min 29.7 MPa (AS
9、TM D 638, 50 mm/min test speed) 3.4.2.1 Elongation at Break, min 25 % 3.4.3 Flexural Yield Strength, min 55 MPa (ASTM D 790, 6.4 x 12.7 mm specimen) 3.4.4 Flexural Modulus, min 2.2 GPa (ASTM D 790, 6.4 x 12.7 mm specimen) 3.4.5 Impact Strength, Izod, min 145 J/m (ASTM D 256) 3.4.6 Heat Deflection Te
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