MIL HDBK 5 : G_VOL2
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
Available format(s)
PDF
Language(s)
English
Publisher
Superseded date
05-05-2004
Superseded by
US$20.00
Excluding Tax where applicable
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
Gives a source of design mechanical and physical properties, and joint allowables.
| Committee |
FSC 1560
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| DevelopmentNote |
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)
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| DocumentType |
Standard
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| Pages |
782
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| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
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| SupersededBy | |
| Supersedes |
| MIL-M-8856 Revision B:1990 | Missiles, Guided, Structural Integrity General Specification for |
| NASA KSC STD Z 0004 : 2002 | STRUCTURAL DESIGN, STANDARD FOR |
| MMPDS 02 : 2005 | METALLIC MATERIALS PROPERTIES DEVELOPMENT AND STANDARDIZATION (MMPDS) |
| MIL-A-8860 Revision B:1987 | Airplane Strength and Rigidity, General Specification for |
| MIL-A-83577 Revision B:1988 | Assemblies, Moving Mechanical, for Space and Launch Vehicles, General Specification for (No S/S Document) |
| MIL-HDBK-337 Base Document:1982 | Adhesive Bonded Aerospace Structure Repair |
| MIL-HDBK-762 Base Document:1990 | Design of Aerodynamically Stabilized Free Rockets |
| MIL-M-8555 Revision C:1984 | Missile, Guided, Design and Construction, General Specification for (No S/S Document) |
| MIL-HDBK-349 Base Document:1994 | 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 29730-1:1989-10 | Aerospace; rivet design values, static load, for universal head rivet joints, single shear; rivet materials 3.1124 and 3.1324 |
| MIL-I-82787 Base Document:1990 | Igniter Assembly, Rocket Motor MK 104 (No S/S Document) |
| MIL-STD-1522 Revision A:1984 | Standard General Requirements for Safe Design and Operation of Pressurized Missile and Space Systems |
| MIL-S-45933 Base Document:1971 | STUD, KEYRING LOCKED, 125 AND 160 KSI FTU, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| NASA KSC STD Z 0005 : 1988 | DESIGN OF PNEUMATIC GROUND-SUPPORT EQUIPMENT, STANDARD FOR |
| BS EN 14607-8:2004 | Space engineering. Mechanical Materials |
| ISO 20312:2011 | Petroleum and natural gas industries — Design and operating limits of drill strings with aluminium alloy components |
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-A-23121 Revision C:1970 | Aircrew Environmental, Escape and Survival Cockpit Capsule System General Specification for (No S/S Document) |
| MIL-B-87114 Revision A:1978 | BOLTS, RECESS DRIVE, GENERAL SPECIFICATION FOR |
| MIL-STD-1312-4 Base Document:1984 | FASTENER TEST METHODS, METHOD 4, LAP JOINT SHEAR (S/S BY NASM1312-4) |
| MIL-R-83459 Revision A:1978 | RIVET, TITANIUM, BIMETAL 95 KSI FSU, GENERAL SPECIFICATION FOR (S/S BY NASM83459) |
| MIL-HDBK-1587 Base Document:1996 | Materials and Process Requirements for Air Force Weapons Systems (S/S by MIL-STD-1587) |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-A-81973 Base Document:1974 | Aircrew Automated Escape Systems, Test Vehicles for Ground Track Performance Testing, Rocket and/or Jet Engine Propelled, General Specification for (No S/S Document) |
| MIL-H-8775 Revision D:1976 | Hydraulic System Components, Aircraft and Missiles General Specification for (S/S by SAE-AS8775) |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MS25420 Revision B:1998 | FASTENERS, STRAIGHT, HEADED, SWAGED COLLAR LIMITATIONS FOR USE OF (S/S BY NASM25420) |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-STD-1312-26 Base Document:1985 | FASTENER TEST METHODS, METHOD 26, STRUCTURAL PANEL FASTENER LAP JOINT SHEAR (S/S BY NASM1312-26) |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-D-23660 Revision A:1965 | Data, Technical for Rocket Motors (No S/S Document) |
| MIL-R-85880 Base Document:1988 | ROCKET, 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 |
| MIL-STD-2156 Base Document:1983 | Launcher, Rail, Guided Missile, Aircraft, General Design Criteria for |
| 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-I-45934 Base Document:1971 | Insert, Screw Thread, Keyring Locked, Self Locking and Non Self Locking, 125, 180, and 220 KSI FTU: General Specification for (No S/S Document) |
| MIL-E-50796 Base Document:1973 | Expanding Shielded Mild Detonating Cord Assembly |
| DIN 29730-3:1989-10 | Aerospace; rivet design values, static load, for universal head rivet joints, single shear; rivet material 3.3354 |
| DEFSTAN 07-85(PT1)/3(2006) : 2006 | DESIGN REQUIREMENTS FOR WEAPONS AND ASSOCIATED SYSTEMS - PART 1: MANDATORY DESIGN REQUIREMENTS |
| MIL-S-8512 Revision D:1974 | Support Equipment, Aeronautical, Special, General Specification for the Design of |
| MIL-I-82826 Base Document:1985 | Igniter Assembly (No S/S Document) |
| MIL-STD-2131 Revision A:1991 | Launcher, Ejection, Guided Missile, Aircraft, General Design Criteria for |
| 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 Revision B:1997 | Bar, Repeatable Release Holdback (RRHB), Aircraft Launching, General Requirement for |
| ASTM G 64 : 1999 | Standard Classification of Resistance to Stress-Corrosion Cracking of Heat-Treatable Aluminum Alloys |
| MIL-S-85510 Base Document:1981 | Seats, Helicopter Cabin, Crashworthy, 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 Revision B:1987 | Airplane Strength and Rigidity Data and Reports (No S/S Document) |
| MIL-F-85596 Base Document:1983 | FIN, RETARDER, AIR INFLATABLE BSU-85/B |
| MIL-S-18471 Revision G:1983 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| MIL-STD-1547 Revision B:1992 | Electronic Parts, Materials, and Processes for Space and Launch 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 AS8860 | Landing Gear Structural Requirements as Listed in the MIL-886X Series of Specifications |
| 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 |
| PREN 6019 : 200P1 | AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - RECOMMENDED PRACTICE FOR R-CURVE AND K[CO] DETERMINATION |
| 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) |
| ASTM G 64 : 1999 : R2005 | Standard Classification of Resistance to Stress-Corrosion Cracking of Heat-Treatable Aluminum Alloys |
| NASA STD 8719.24 : 2011 | NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS |
| NASA MSFC STD 486 : 1992 | STANDARD, THREADED FASTENERS, TORQUE LIMITS FOR |
| DIN 29730-6:1989-10 | Aerospace; rivet calculation values static load, for universal head rivet joints, double shear; rivet material 2.4360 |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MIL-I-85889 Base Document:1988 | IGNITER, JET ASSISTED TAKE OFF (JATO) PROPULSION SYSTEM, GENERAL DEVELOPMENT SPECIFICATION FOR |
| 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-58095 Revision A:1986 | SEAT SYSTEM: CRASH RESISTANT, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT) |
| MIL-S-81771 Revision A:1975 | Seat System; Aircrew, Crash Resistant; General Specification for |
| 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 Revision A:1980 | PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR |
| MIL-I-8671 Revision D:1994 | Installation of Droppable Stores and Associated Release Systems |
| MIL-R-23139 Revision B:1965 | Rocket Motors, Surface Launched, Development and Qualification Requirements For |
| MIL-T-18232 Revision B:1968 | Targets, Aerial, Powered, Design and Construction of General Specification for (No S/S Document) |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| MIL-S-48405 Base Document:1973 | Shielded and Confined Mild Detonating Cord Assemblies |
| DIN 29730-5:1989-10 | Aerospace; rivet values static load, for universal head rivet joints, single shear; rivet material 2.4360 |
| ASTM E 1997 : 2015 : REDLINE | Standard Practice for the Selection of Spacecraft Materials |
| SAE AIR5052A | Crack Initiation and Growth Considerations for Landing Gear Steel With Emphasis on Aermet 100 |
| 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 14607-7:2004 | Space engineering. Mechanical Mechanical parts |
| EN 14607-7:2004 | Space engineering - Mechnical - Part 7: Mechnical 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) |
| MIL-HDBK-60 Base Document:1990 | 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 |
| 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 |
| DOD-HDBK-343 Base Document:1986 | Design, Construction, and Testing Requirements for one of a Kind Space Equipment (No S/S Document) |
| 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 29731-6:1989-10 | Aerospace; rivet design values static load, for countersunk rivet joints, single shear, dimpled; rivet material 2.4360 |
| 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 |
| NASA MSFC STD 506 : 1988 | MATERIALS AND PROCESSES CONTROL |
| SAE AIR4728 | References, Spacecraft and Spacecraft Servicing, Fluid System Components (Abbreviations, Acronyms, Definitions, Applicable Documents and Environmental Conditions) |
| 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 ARP4945A | Aerospace-Solenoid Valve, Hydraulic, Three Way, Two Position, Direct Acting |
| 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 |
| 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 |
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