ARMY MIL-DTL-46063 H-1998 ARMOR PLATE ALUMINUM ALLOY 7039《7039铝合金装甲板》.pdf
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1、MIL-DTL-4bOb3H m 9999906 2073353 390 m Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Director, US Army Research Laboratory, Weapons and Materials Research Directorate, ATTN: AMSRL-WM-M, Aberde
2、en Proving Ground, MD 21005-5069 by using the Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. I INCH-POUND I MIL-DTL- 4 60 63H 14 September 1998 SUPERSEDING MIL-A- 4 60 63G 30 December 1992 DETAI L S PEC I FI CAT I ON ARMOR PLATE, ALUM
3、INUM ALLOY, 7039 This specification is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification covers 7039 wrought aluminum alloy armor plate. The nominal thickness of armor plate covered by this specification is 1/2 inch to 4 inches, inc
4、lusive (see 3.7 and 6.2). 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3 and 4 of this specification. This section does not include documents in other sections of this specification or recommended for additional information or as examples. While
5、 every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed. 2.2 Government documents. 2.2.1 Specifications, standards, and h
6、andbooks. The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the issue of the Department ofDefense Index of Specifications and Standards (DoDISS) and supplem
7、ent thereto, cited in the solicitation (see 6.2). STAN DARDS DEPARTMENT OF DEFENSE MIL-STD-662 - V50 Ballistic Test For Armor (Unless otherwise indicated, copies of the above specifications, standards, and handbooks are available from the Defense Automated Printing Service (DAPS), Bldg. 4D, 700 Robb
8、ins Avenue, Philadelphia, PA 19111-5094.) AMSC N/A FSC 9535 Licensed by Information Handling Servicesm 90b 2073354 227 m MIL-DTL-46063H 2.3 Non-Government publications. The following documents form a part of this specification to the extent specified herein. Unless otherwise specified, the issues of
9、 the documents which ire DoD adopted are those listed in the issue of the DoDISS cited in the solicitation. Unless otherwise specified, the issues of documents not listed in the DoDISS are the issues of the documents cited in the solicitation (see 6.2). AMERICAN NATIONAL STANDARDS INSTITUTE (ANSI) A
10、NSI H35.2 - Dimensional Tolerances for Aluminum Mill Products (DoD adopted) (Application for copies should be addressed to the American National Standards Institute, 11 West 42nd Street, New York, NY 10036.) AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM B557 ASTM E34 ASTM E227 ASTM E607 AST
11、M E716 ASTM E1251 ASTM G38 ASTM G47 Tension Testing Wrought and Cast Aluminum and Magnesium- Alloy Products (DoD adopted) Chemical Analysis of Aluminum and Aluminum-Base Alloys (DoD adopted) Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique (DoD
12、adopted) Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Point-to-Plane Technique, Nitrogen Atmosphere (DoD adopted) Sampling Aluminum and Aluminum Alloys for Spectrochemical Analysis Optical Emission Spectrometric Analysis of Aluminum and Aluminum Alloys by the Argon
13、Atmosphere, Point-to-Plane, Unipolar Self-Initiating Capacitor Discharge (DoD adopted) Making and Using C-Ring Stress-Corrosion Test Specimens (DoD adopted) Determining Susceptibility to Stress-Corrosion Cracking of High Strength Aluminum Alloy Products (DoD adopted) (Application for copies should b
14、e addressed to the American Society for Testing and Materials, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.) 2.4 Order of precedence. In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this
15、document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 First article. When specified in the contract or purchase order (see 6.2) and before production has commenced, samples of the specified item shall be made available to the
16、 contracting officer or his authorized representative for approval in accordance with 4.3.1. The approval of the first article samples authorizes the commencement of production but does not relieve the supplier of responsibility for compliance with all applicable provisions of this specification. Th
17、e first article samples shall be manufactured by the process proposed for use on production. 2 Licensed by Information Handling ServicesflIL-DTL-46063H 9999906 2073355 Lb3 M MIL-DTL-46063H 3.2 Chemical cornposition. Chemical composition shall be within the limits shown in table I. A certification of
18、 the chemical composition of the alloy shall be furnished with the ballistic test plates (see 6.2). TABLE I. Chemical composition. Element Percent Zinc Ma gne s ium Manganes e Copper I ron Silicon Chromium Titanium Others, each Others, total Aluminum (by difference) 3.5 - 4.5 2.3 - 3.3 0.10 - 0.40 .
19、10 max .40 max .30 max .10 max .OS max .15 max Rema i nde r .15 - 0.25 3.3 Mechanical properties. Unless otherwise specified in the contract or order (see 6.21, the mechanical properties of.the test specimen taken in the long-transverse direction shall meet the requirements of table II when tested a
20、s specified in 4.7.2. table II, or if any other properties are required and if the difference in properties are negotiated between the procuring activity and the supplier, the minimum acceptable ballistic requirements of appendix A will apply. If mechanical properties differ from the values shown in
21、 TABLE II. Mechanical properties. Yield Elongation strength 0.2% offset, percent in Tensile strength min, Thickness, inch min, psi min, psi 2 in. Up to 1.500, incl Over 1.500 60,000 51,000 57,000 48,000 9 8 3.4 Stress corrosion resistance. Unless otherwise specified in the contract or order (see 6.2
22、), plate material 0.72 inch and thicker in the short transverse direction shall be resistant to stress corrosion cracking. A minimum of 5 of the 9 specimens tested shall show no evidence of cracking at the end of 96 hours when tested as specified in 4.7.3 (see 6.4). 3.5 Heat treatment. Heat treatmen
23、t shall be such as to meet the requirements of this specification (see 6.5). 3.6 Ballistic limit. The protection ballistic limit, BL(P), shall be as specified in appendix A. 3 Licensed by Information Handling ServicesMIL-DTL-46063H = 9999906 2073356 OTT MIL-DTL-46063H , 3.7 Dimensions. Dimensions sh
24、all be as specified in the contract or order (see 6.2). 3.7.1 Tolerances. Unless otherwise specified in the contract or order (see 6.21, the plates submitted for acceptance shall not vary from the specified dimensions by an amount greater than the tolerances shown in ANSI H35.2. Ballistic test plate
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