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  • MIL HDBK 5 : G_VOL2

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    METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES

    Available format(s):  Hardcopy, PDF

    Superseded date:  05-05-2004

    Language(s):  English

    Published date: 

    Publisher:  US Military Specs/Standards/Handbooks

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    Table of Contents - (Show below) - (Hide below)

    Chapter 1. General
    1.1 Purpose and use of document
    1.2 Symbols, abbreviations, and systems of units
    1.3 Commonly used formulas
    1.4 Basic principles and definitions
    1.5 Types of failures
    1.6 Columns
    1.7 Thin-walled and stiffened
    References
    Chapter 2. Steel
    2.1 General
    2.2 Carbon steels
    2.3 Low-alloy steel (AISI grades and proprietary
          grades)
    2.4 Intermediate alloy steels
    2.5 High-alloy steels
    2.6 Precipitation and transformation-hardening steels
          (stainless)
    2.7 Austenitic stainless steels
    2.8 Element properties
    References
    Chapter 3. Aluminum
    3.1 General
    3.2 2000 series wrought alloys
    3.3 3000 series wrought alloys
    3.4 4000 series wrought alloys
    3.5 5000 series wrought alloys
    3.6 6000 series wrought alloys
    3.7 7000 series wrought alloys
    3.8 200.0 series cast alloys
    3.9 300.0 series cast alloys
    3.10 500.0 series cast alloys
    3.11 Element properties
    References
    Chapter 4. Magnesium alloys
    4.1 General
    4.2 Magnesium alloy wrought products
    4.3 Magnesium alloy cast products
    4.4 Element properties
    References
    Chapter 5. Titanium
    5.1 General
    5.2 Unalloyed titanium
    5.3 Alpha and near-alpha titanium alloys
    5.4 Alpha beta titanium alloys
    5.5 Beta, near-beta, and metastable-beta titanium
          alloys
    5.6 Element properties
    References
    Chapter 6. Heat-resistant alloys
    6.1 General
    6.2 Iron-chromium-nickel-base alloys
    6.3 Nickel-base alloys
    6.4 Cobalt-base alloys
    References
    Chapter 7. Miscellaneous alloys and hybrid materials
    7.1 General
    7.2 Beryllium
    7.3 Copper and copper alloys
    7.4 Multiphase alloys
    7.5 Aluminum alloy sheet laminates
    References
    Chapter 8. Structural joints
    8.1 Mechanically fastened joints
    8.2 Metallurgical joints
    8.3 Bearings, pulleys, and wire rope
    References
    Chapter 9. Guidelines for the presentation of data
    9.1 General
    9.2 Room-temperature design allowables
    9.3 Graphical mechanical-property data
    9.4 Properties of joints and structures
    9.5 Miscellaneous properties
    9.6 Statistical procedures and tables
    References

    Abstract - (Show below) - (Hide below)

    Gives a source of design mechanical and physical properties, and joint allowables.

    General Product Information - (Show below) - (Hide below)

    Committee FSC 1560
    Development Note J Notice 1 - Notice of Cancellation/Superseded by DOT/FAA/AR-MMPDS-01 (05/2004) J NOTICE 2 - Notice of Cancellation/Superseded by DOT/FAA/AR-MMPDS-01 (04/2006)
    Document Type Standard
    Publisher US Military Specs/Standards/Handbooks
    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    DIN 29730-6:1989-10 Aerospace; rivet calculation values static load, for universal head rivet joints, double shear; rivet material 2.4360
    MIL D 23660 : A DATA, TECHNICAL FOR ROCKET MOTORS
    MIL R 85880 : 0 ROCKET, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR
    JSSG 2006 : 0 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
    MIL I 85889 : 0 IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR
    03/301400 DC : DRAFT JAN 2003 EN 14607-8 - SPACE ENGINEERING - MECHANICAL - PART 8: MATERIALS
    SAE ARP 1281 : 2002 ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR
    MIL M 8856 : B MISSILE, GUIDED, STRUCTURAL INTEGRITY, GENERAL SPECIFICATION FOR
    MIL HDBK 60 : 0 THREADED FASTENERS - TIGHTENING TO PROPER TENSION
    DIN 65736-3:1984-03 Aerospace; bolt calculation values, static load, for countersunk head bolts, single shear, bolt material 1.7220.5
    I.S. EN 14607-8:2004 SPACE ENGINEERING - MECHANICAL - PART 8: MATERIALS
    DIN 29734-8:1989-10 Aerospace; rivet design values static load, for blind rivets according to MS 20600AD with protruding head, single shear
    MIL S 85510 : 0
    I.S. EN 14607-7:2004 SPACE ENGINEERING - MECHANICAL - PART 7: MECHANICAL PARTS
    DIN 29730-4:1989-10 Aerospace; rivet design values, static load, for universal head rivet joints, double shear; rivet material 3.3354
    MIL A 8860 : B AIRPLANE STRENGTH AND RIGIDITY GENERAL SPECIFICATION FOR
    MIL A 83577 : B ASSEMBLIES, MOVING MECHANICAL, FOR SPACE AND LAUNCH VEHICLES, GENERAL SPECIFICATION FOR
    MIL HDBK 337 : 0 ADHESIVE BONDED AEROSPACE STRUCTURE REPAIR
    UNI EN ISO 20312 : 2011 PETROLEUM AND NATURAL GAS INDUSTRIES - DESIGN AND OPERATING LIMITS OF DRILL STRINGS WITH ALUMINIUM ALLOY COMPONENTS
    MIL I 45934 : 0 INSERT, SCREW THREAD, KEYRING LOCKED, SELF LOCKING AND NON SELF LOCKING, 125, 180, AND 220 KSI FTU: GENERAL SPECIFICATION FOR
    SAE AS 85075 : 2000 TIE DOWN ASSEMBLY, HELICOPTER BLADE, GENERAL SPECIFICATION FOR
    MIL F 81836 : A SUPP 1 FILTER AND DISPOSABLE ELEMENT, FLUID PRESSURE, HYDRAULIC, 3 MICRON ABSOLUTE
    MIL S 58095 : A SEAT SYSTEM: CRASH RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR
    DIN 29731-1:1989-10 Aerospace; rivet design values static load, for countersunk rivet joints, single shear; rivet materials 3.1124 and 3.1324
    MIL A 8868 : B AIRPLANE STRENGTH AND RIGIDITY DATA AND REPORTS
    MIL HDBK 762 : 0 DESIGN OF AERODYNAMICALLY STABILIZED FREE ROCKETS
    DOD HDBK 343 : 0 DESIGN, CONSTRUCTION, & TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT
    MIL S 81771 : A SEAT SYSTEM; AIRCREW, CRASH RESISTANT; GENERAL SPECIFICATION FOR
    MIL F 85596 : 0 FIN, RETARDER, AIR INFLATABLE BSU-85/B
    MIL E 50796 : 0 EXPANDING SHIELDED MILD DETONATING CORD ASSEMBLY
    MIL M 8555 : C MISSILE, GUIDED, DESIGN AND CONSTRUCTION, GENERAL SPECIFICATION
    MIL HDBK 349 : 0 MANUFACTURE AND INSPECTION OF ADHESIVE BONDED, ALUMINUM HONEYCOMB SANDWICH ASSEMBLIES FOR AIRCRAFT
    DIN 29731-51:1989-10 Aerospace; rivet design values static load, for countersunk rivet joints, single shear, dimpled; rivet materials 3.1124 and 3.1324
    DIN 65736-5:1984-03 Aerospace; bolt calculation values, static load, for countersunk head bolts, single shear, bolt materials 1.4944.4 and 1.7734.5
    DIN 29730-3:1989-10 Aerospace; rivet design values, static load, for universal head rivet joints, single shear; rivet material 3.3354
    DIN 29731-6:1989-10 Aerospace; rivet design values static load, for countersunk rivet joints, single shear, dimpled; rivet material 2.4360
    DIN 65736-7:1984-03 Aerospace; bolt calculation values, static load, for countersunk head bolts, single shear, bolt material 1.6604.6
    MIL P 83126 : A PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR
    MIL I 8671 : D INSTALLATION OF DROPPABLE STORES AND ASSOCIATED RELEASE SYSTEMS
    MIL S 18471 : G
    MIL STD 1547 : B ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE VEHICLES
    DIN 29731-52:1989-10 Aerospace; rivet design values static load, for countersunk rivet joints, double shear, dimpled; rivet materials 3.1124 and 3.1324
    SAE AS 8860 : 2012 LANDING GEAR STRUCTURAL REQUIREMENTS AS LISTED IN THE MIL-886X SERIES OF SPECIFICATIONS
    DEFSTAN 07-85(PT1)/3(2006) : 2006 DESIGN REQUIREMENTS FOR WEAPONS AND ASSOCIATED SYSTEMS - PART 1: MANDATORY DESIGN REQUIREMENTS
    DIN 29730-1:1989-10 Aerospace; rivet design values, static load, for universal head rivet joints, single shear; rivet materials 3.1124 and 3.1324
    DIN 65494-101:1989-10 Aerospace; rivet design values, static load, for protruding head rivet joints, single shear; rivet material 3.1124, metric series
    03/301399 DC : DRAFT JAN 2003 EN 14607-7 - SPACE ENGINEERING - MECHANICAL - PART 7: MECHANICAL PARTS
    BS EN ISO 20312:2011 Petroleum and natural gas industries. Design and operating limits of drill strings with aluminium alloy components
    MIL R 23139 : B ROCKET MOTORS, SURFACE LAUNCHED, DEVELOPMENT AND QUALIFICATION REQUIREMENTS FOR
    MIL T 18232 : B TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR
    MIL A 87221 : 0 AIRCRAFT STRUCTURES, GENERAL SPECIFICATION FOR REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503
    MIL S 8512 : D SUPPORT EQUIPMENT AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF
    MIL I 82787 : 0 IGNITER ASSEMBLY, ROCKET MOTOR MK 104
    MIL STD 1522 : A STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS
    NASA MSFC STD 506 : 1988 MATERIALS AND PROCESSES CONTROL
    SAE AIR 4728 : 2013 REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS)
    JSSG 2010 12 : 0 CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK
    MIL S 48405 : 0 SHIELDED AND CONFINED MILD DETONATING CORD ASSEMBLIES
    MIL I 82826 : 0 IGNITER ASSEMBLY
    MIL STD 2131 : A LAUNCHER, EJECTION GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR
    MIL S 45933 : 0 STUD, KEYRING LOCKED, 125 AND 160 KSI FTU, GENERAL SPECIFICATION FOR
    S157-17/S157.1-17 Strength design in aluminum / Commentary on CSA S157-17, Strength design in aluminum
    DIN 29730-5:1989-10 Aerospace; rivet values static load, for universal head rivet joints, single shear; rivet material 2.4360
    PREN 6019 : 200P1 AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - RECOMMENDED PRACTICE FOR R-CURVE AND K[CO] DETERMINATION
    PREN 6074 : 200P1 AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - STATISTICAL DATA FOR MATERIAL QUALIFICATION
    DIN 65495-201:1990-08 Aerospace; rivet design values, static load, for flush head rivet joints, single shear, dimpled, rivet material 3.1124, metric series
    DIN 29735-8:1989-10 Aerospace; rivet design values static load, for blind rivets according to MS 20601AD with countersunk head, single shear
    MIL DTL 85110 : B BAR, REPEATABLE RELEASE HOLDBACK (RRHB), AIRCRAFT LAUNCHING, GENERAL REQUIREMENT FOR
    NASA KSC STD Z 0005 : 1988 DESIGN OF PNEUMATIC GROUND-SUPPORT EQUIPMENT, STANDARD FOR
    DIN 65736-1:1984-03 Aerospace; bolt calculation values, static load, for countersunk head bolts, single shear, bolt materials 1.1174.7 and 1.4544.9
    DIN 29731-5:1989-10 Aerospace; rivet design values static load, for countersunk rivet joints, single shear; rivet material 2.4360
    SAE ARP 4945 : 2013 AEROSPACE-SOLENOID VALVE, HYDRAULIC, THREE WAY, TWO POSITION, DIRECT ACTING
    ASTM E 1997 : 2015 : REDLINE Standard Practice for the Selection of Spacecraft Materials
    I.S. EN ISO 20312:2011 PETROLEUM AND NATURAL GAS INDUSTRIES - DESIGN AND OPERATING LIMITS OF DRILL STRINGS WITH ALUMINIUM ALLOY COMPONENTS (ISO 20312:2011)
    SAE AIR 5052 : 1997 CRACK INITIATION AND GROWTH CONSIDERATIONS FOR LANDING GEAR STEEL WITH EMPHASIS ON AERMET 100
    API TR 17TR8 : 2018 HIGH-PRESSURE HIGH-TEMPERATURE DESIGN GUIDELINES
    ASTM G 64 : 1999 : R2013 Standard Classification of Resistance to Stress-Corrosion Cracking of Heat-Treatable Aluminum Alloys
    ASTM G 64 : 1999 : R2005 Standard Classification of Resistance to Stress-Corrosion Cracking of Heat-Treatable Aluminum Alloys
    MIL STD 2156 : 0 LAUNCHER, RAIL, GUIDED MISSILE, AIRCRAFT, GENERAL DESIGN CRITERIA FOR
    NASA KSC STD Z 0004 : 2002 STRUCTURAL DESIGN, STANDARD FOR
    MMPDS 02 : 2005 METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS)
    ASTM G 64 : 1999 Standard Classification of Resistance to Stress-Corrosion Cracking of Heat-Treatable Aluminum Alloys
    DIN 29735-6:1989-10 Aerospace; rivet design values static load, for blind rivets according to NAS 1399D with countersunk head, single shear
    DIN 29732-1:1984-03 Aerospace; rivet calculation values, static load, for close tolerance rivets of steel with universal head, single shear
    DIN 29733-1:1984-03 Aerospace; rivet calculation values, static load, for close tolerance rivets of steel, with countersunk head, single shear
    DIN 29734-6:1989-10 Aerospace; rivet design values static load, for blind rivets according to NAS 1398D with protruding head, single shear
    BS EN 14607-8 : 2004 SPACE ENGINEERING - MECHANICAL - PART 8: MATERIALS
    BS EN 14607-7 : 2004 SPACE ENGINEERING - MECHANICAL - PART 7: MECHANICAL PARTS
    ISO 20312:2011 Petroleum and natural gas industries Design and operating limits of drill strings with aluminium alloy components
    NASA STD 8719.24 : 2011 NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS
    NASA MSFC STD 486 : 1992 STANDARD, THREADED FASTENERS, TORQUE LIMITS FOR
    EN 14607-7 : 2004 SPACE ENGINEERING - MECHANICAL - PART 7: MECHANICAL PARTS
    EN 14607-8 : 2004 SPACE ENGINEERING - MECHANICAL - PART 8: MATERIALS
    EN ISO 20312 : 2011 PETROLEUM AND NATURAL GAS INDUSTRIES - DESIGN AND OPERATING LIMITS OF DRILL STRINGS WITH ALUMINIUM ALLOY COMPONENTS (ISO 20312:2011)
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