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DEFSTAN 95-31/1(2002) : 2002

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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ALUMINIUM ALLOY ARMOUR PLATE (7019)

Published date

12-01-2013

Superseded date

03-09-2004

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Description Page
Content
Preface
Main Text
SECTION 1 GENERAL REQUIREMENTS
0 Introduction
1 Scope
2 WARNING
3 Related Documents
4 Definitions
5 General
6 Basis of Specification
7 Precautionary Note on Stress Corrosion Cracking
8 Precautionary Note on Bending
SECTION 2 MATERIAL VALIDATION
9 Material Requirements
10 Documentation
SECTION 3 PRODUCTION REQUIREMENTS
11 Production Plate Requirements
Table 1 Ballistic Test Ammunition
Table 2 Mechanical Property Requirements
Table 3 Minimum Number of Tensile Tests
Table 4 Chemical Composition
Table 5 Test Weld Data
Table 6 Class "A" Thickness Tolerances
Table 7 Class "B" Thickness Tolerances
Fig 1 Cruciform Test Piece
Fig 2 Vee-Groove Weld Test Piece
Fig 3 Pattern of Liquation Cracks
Fig 4 Stress Corrosion Test Piece
Fig 5 Test Piece Orientation

Specifies the material and performance requirements for a weldable aluminium alloy armour plate, 6 mm and above, of nominal 4% Zinc 2% Magnesium Aluminium alloy in the solution treated and aged condition for the protection of crew and mechanism of armoured fighting vehicles against attack.

DocumentType
Standard
PublisherName
UK Ministry of Defence Standards
Status
Superseded
SupersededBy

DEFSTAN 95-32/1(2002) : 2002 ALUMINIUM ALLOY ARMOUR EXTRUSIONS AND FORGINGS (7019)

DEFSTAN 08-42/1(2000) : 2000 ARMOUR PROOF, BALLISTIC TEST METHODOLOGY
ASTM G 85 : 2011 : REDLINE Standard Practice for Modified Salt Spray (Fog) Testing
DEFSTAN 08-39/1(1998) : 1998 CUTTING, WELDING AND CORROSION PROTECTION OF ALUMINIUM ALLOY MILITARY EQUIPMENT
DEFSTAN 95-22/1(1997) : 1997 ALUMINIUM ALLOY ARMOUR PLATE (HEAT TREATABLE 6-120 MM)
BS EN 485-3:2003 Aluminium and aluminium alloys. Sheet, strip and plate Tolerances on dimensions and form for hot-rolled products
LN 65666:1974-07 Stress-corrosion cracking test of wrought aluminium alloys for aircraft
BS EN 485-1 : 2008 ALUMINIUM AND ALUMINIUM ALLOYS - SHEET, STRIP AND PLATE - PART 1: TECHNICAL CONDITIONS FOR INSPECTION AND DELIVERY
BS EN 10002-1:2001 Tensile testing of metallic materials Method of test at ambient temperature

Sorry this product is not available in your region.