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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Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

METALLIC MATERIALS AND ELEMENTS FOR AEROSPACE VEHICLE STRUCTURES
Available format(s)

PDF

Superseded date

05-05-2004

Language(s)

English

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
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)
DocumentType
Standard
Pages
782
PublisherName
US Military Specs/Standards/Handbooks
Status
Superseded
SupersededBy
Supersedes

SAE ARP 1281 : 2002 ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR
MIL-M-8856 Revision B:1990 MISSILE, 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
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
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
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
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
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
MIL-R-83459 Revision A:1978 RIVET, TITANIUM, BIMETAL 95 KSI F SU GENERAL SPECIFICATION FOR
MIL-HDBK-1587 Base Document:1996 MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM
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
MIL-H-8775 Revision D:1976 HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR
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 PIN, STRAIGHT, HEADED, SWAGED COLLAR, LIMITATIONS FOR USE OF (ASG)
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
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
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
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
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
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
MIL-F-85596 Base Document:1983 FIN, RETARDER, AIR INFLATABLE BSU-85/B
MIL-S-18471 Revision G:1983
MIL-STD-1547 Revision B:1992 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
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 JOINT SERVICE SPECIFICATION GUIDE - 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 RESISTANCE, NON-EJECTION, AIRCREW, GENERAL SPECIFICATION FOR
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 TARGET, AERIAL, POWERED, DESIGN AND CONSTRUCTION OF GENERAL SPECIFICATION FOR
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 AIR 5052 : 1997 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
UNI EN ISO 20312 : 2011 PETROLEUM AND NATURAL GAS INDUSTRIES - DESIGN AND OPERATING LIMITS OF DRILL STRINGS WITH ALUMINIUM ALLOY COMPONENTS
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, & TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT
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 AIR 4728 : 2013 REFERENCES, SPACECRAFT AND SPACECRAFT SERVICING, FLUID SYSTEM COMPONENTS (ABBREVIATIONS, ACRONYMS, DEFINITIONS, APPLICABLE DOCUMENTS AND ENVIRONMENTAL CONDITIONS)
S157-17/S157.1-17 Strength design in aluminum / Commentary on CSA S157-17, Strength design in aluminum
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
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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