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DEFSTAN 95-31/2(2004) : 2004

Withdrawn

Withdrawn

ALUMINIUM ALLOY ARMOUR PLATE (7019)

Published date

01-12-2013

Withdrawn date

03-30-2011

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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
ANNEX A Ballistic Assessment
ANNEX B Mechanical Properties
ANNEX C Chemical Composition
ANNEX D Weldability
ANNEX E Long Transverse Stress Corrosion Resistance
ANNEX F Short Transverse Stress Corrosion Resistance
ANNEX G Dimensional Tolerances
ANNEX H Workmanship
ANNEX I Identification
ANNEX J Bending

Defines 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.

DevelopmentNote
Supersedes DEFSTAN 95-31/1(2002). (10/2004)
DocumentType
Standard
PublisherName
UK Ministry of Defence Standards
Status
Withdrawn
Supersedes

DEFSTAN 95-32/2(2004) : 2004 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 95-32/1(2002) : 2002 ALUMINIUM ALLOY ARMOUR EXTRUSIONS AND FORGINGS (7019)
DEFSTAN 08-202/1(2002) : 2002 BALLISTIC TABLES FOR DEFENCE STANDARD 95-31
BS EN 485-3:2003 Aluminium and aluminium alloys. Sheet, strip and plate Tolerances on dimensions and form for hot-rolled products
DEFSTAN 95-22/4(2004) : 2004 ALUMINIUM ALLOY ARMOUR PLATE (HEAT TREATABLE 6-120 MM)
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.