MIL-HDBK-17-3 Revision F:2002
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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COMPOSITE MATERIALS HANDBOOK - VOLUME 3: POLYMER MATRIX COMPOSITES MATERIALS USAGE, DESIGN, AND ANALYSIS
26-03-2013
Foreword
Summary of Changes
CHAPTER 1 - GENERAL INFORMATION
1.1 INTRODUCTION
1.2 PURPOSE, SCOPE, AND ORGANIZATION OF VOLUME 3
1.3 SYMBOLS, ABBREVIATIONS, AND SYSTEM OF UNITS
CHAPTER 2 - MATERIALS AND PROCESSES - THE EFFECT OF
VARIABILITY ON COMPOSITE PROPERTIES
2.1 INTRODUCTION
2.2 PURPOSE
2.3 SCOPE
2.4 CONSTITUENT MATERIALS
2.5 PROCESSING OF PRODUCT FORMS
2.6 SHIPPING AND STORAGE PROCESSES
2.7 CONSTRUCTION PROCESSES
2.8 CURE AND CONSOLIDATION PROCESSES
2.9 ASSEMBLY PROCESSES
2.10 PROCESS CONTROL
2.11 PREPARING MATERIAL AND PROCESSING
SPECIFICATIONS
REFERENCES
CHAPTER 3 - QUALITY CONTROL OF PRODUCTION MATERIALS
3.1 INTRODUCTION
3.2 QUALITY ASSURANCE PROCEDURES
3.3 MATERIAL PROPERTY VERIFICATION
3.4 STATISTICAL PROCESS CONTROL
REFERENCES
CHAPTER 4 - DESIGN AND ANALYSIS
4.1 INTRODUCTION
4.2 BASIC LAMINA PROPERTIES AND MICROMECHANICS
4.3 ANALYSIS OF LAMINATES
4.4 LAMINATE STRENGTH AND FAILURE
4.5 COMPLEX LOADS
4.6 LAMINA TO LAMINATE CONSIDERATIONS
4.7 COMPRESSIVE BUCKLING AND CRIPPLING
4.8 CARPET PLOTS
4.9 CREEP AND RELAXATION
4.10 FATIGUE
4.11 OTHER STRUCTURAL PROPERTIES
4.12 VIBRATION
4.13 COMPUTER PROGRAMS
4.14 CERTIFICATION REQUIREMENTS
REFERENCES
CHAPTER 5 - STRUCTURAL BEHAVIOUR OF JOINTS
5.1 INTRODUCTION
5.2 ADHESIVE JOINTS
5.3 MECHANICALLY FASTENED JOINTS
REFERENCES
CHAPTER 6 - STRUCTURAL RELIABILITY
6.1 INTRODUCTION
6.2 FACTORS AFFECTING STRUCTURAL RELIABILITY
6.3 RELIABILITY ENGINEERING
6.4 RELIABILITY DESIGN CONSIDERATIONS
6.5 RELIABILITY ASSESSMENT AND DESIGN
REFERENCES
CHAPTER 7 - THICK SECTION COMPOSITES
7.1 INTRODUCTION
7.2 MECHANICAL PROPERTIES REQUIRED FOR THICK
SECTION COMPOSITE THREE-DIMENSIONAL ANALYSIS
7.3 STRUCTURAL ANALYSIS METHOD FOR THICK-SECTION
COMPOSITES
7.4 PHYSICAL PROPERTY ANALYSIS REQUIRED FOR
THICK-SECTION COMPOSITE THREE-DIMENSIONAL
ANALYSIS
7.5 PROCESS ANALYSIS METHODS FOR THICK-SECTION
COMPOSITES
7.6 FAILURE CRITERIA
7.7 FACTORS INFLUENCING THICK-SECTION ALLOWABLES
(I.E., SAFETY MARGINS)
7.8 THICK LAMINATE DEMONSTRATION PROBLEM
REFERENCES
CHAPTER 8 - SUPPORTABILITY
8.1 INTRODUCTION
8.2 DESIGN FOR SUPPORTABILITY
8.3 SUPPORT IMPLEMENTATION
8.4 LOGISTICS REQUIREMENTS
8.5 TERMINOLOGY
REFERENCES
CHAPTER 9 - LESSONS LEARNED
9.1 INTRODUCTION
9.2 UNIQUE ISSUES FOR COMPOSITES
9.3 LESSONS LEARNED
REFERENCES
INDEX
Gives the methodologies and lessons learned for the design, manufacture and analysis of composite structures and for utilization of the material data given in Volume 2 consistent with the guidance given in Volume 1.
Committee |
AREA CMPS
|
DevelopmentNote |
F NOTICE 1 - Notice of Cancellation/Superseded by SAE R-424. (04/2013)
|
DocumentType |
Standard
|
Pages |
694
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Superseded
|
SupersededBy |
ASCE/SEI 59 11 : 2011 | BLAST PROTECTION OF BUILDINGS |
ASTM D 7766/D7766M : 2016 : REDLINE | Standard Practice for Damage Resistance Testing of Sandwich Constructions |
ASTM D 7136/D7136M : 2015 : REDLINE | Standard Test Method for Measuring the Damage Resistance of a Fiber-Reinforced Polymer Matrix Composite to a Drop-Weight Impact Event |
ASTM D 6264/D6264M : 2017 : REDLINE | Standard Test Method for Measuring the Damage Resistance of a Fiber-Reinforced Polymer-Matrix Composite to a Concentrated Quasi-Static Indentation Force |
DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
DEFSTAN 00-970(PT1)SEC3/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
DEFSTAN 00-970(PT1)SEC3/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
NASA STD 6016(INT) : 2006 | STANDARD MATERIALS AND PROCESSES REQUIREMENTS FOR SPACECRAFT |
NASA KSC DE 512-SM : 2012 | FACILITY SYSTEMS, GROUND SUPPORT SYSTEMS, AND GROUND SUPPORT EQUIPMENT GENERAL DESIGN REQUIREMENTS |
DEFSTAN 00-970(PT1)SEC3/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
DEFSTAN 00-970(PT1)SEC3/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
DEFSTAN 00-970(PT1)SEC3/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE |
ASME RTP 1 : 2015 | REINFORCED THERMOSET PLASTIC CORROSION-RESISTANT EQUIPMENT |
ASME RTP-1 : 2017 | REINFORCED THERMOSET PLASTIC CORROSION-RESISTANT EQUIPMENT |
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