NOT MEASUREMENT SENSITIVE MIL-HDBK-17-3F Volume 3 of 5 17JUNE2002 Superseding MIL-HDBK-17-3E 23 JANUARY 1997 DEPARTMENT OF DEFENSE HANDBOOK COMPOSITE MATERIALS HANDBOOK VOLUME 3.POLYMER MATRIX COMPOSITES MATERIALS USAGE,DESIGN,AND ANALYSIS ITED This handbook is for guidance only.Do not cite this document as a requirement. AMSC N/A AREA CMPS DISTRIBUTION STATEMENT A.Approved for public release;distribution unlimited
NOT MEASUREMENT SENSITIVE MIL-HDBK-17-3F Volume 3 of 5 17 JUNE 2002 Superseding MIL-HDBK-17-3E 23 JANUARY 1997 DEPARTMENT OF DEFENSE HANDBOOK COMPOSITE MATERIALS HANDBOOK VOLUME 3. POLYMER MATRIX COMPOSITES MATERIALS USAGE, DESIGN, AND ANALYSIS This handbook is for guidance only. Do not cite this document as a requirement. AMSC N/A AREA CMPS DISTRIBUTION STATEMENT A. Approved for public release; distribution unlimited
MIL-HDBK-17-3F Volume 3.Foreword Table of Contents FOREWORD 1.This Composite Materials Handbook Series,MIL-HDBK-17,are approved for use by all Departments and Agencies of the Department of Defense. 2.This handbook is for guidance only.This handbook cannot be cited as a requirement.If it is,the con- tractor does not have to comply.This mandate is a DoD requirement only;it is not applicable to the Federal Aviation Administration(FAA)or other government agencies. 3.Every effort has been made to reflect the latest information on polymer(organic),metal,and ceramic composites.The handbook is continually reviewed and revised to ensure its completeness and cur- rentness.Documentation for the secretariat should be directed to:Materials Sciences Corporation, MIL-HDBK-17 Secretariat,500 Office Center Drive,Suite 250,Fort Washington,PA 19034. 4.MIL-HDBK-17 provides guidelines and material properties for polymer(organic),metal,and ceramic matrix composite materials.The first three volumes of this handbook currently focus on,but are not limited to,polymeric composites intended for aircraft and aerospace vehicles.Metal matrix compos- ites (MMC)and ceramic matrix composites (CMC),including carbon-carbon composites (C-C)are covered in Volume 4 and Volume 5,respectively. 5. This standardization handbook has been developed and is being maintained as a joint effort of the Department of Defense and the Federal Aviation Administration. 6.The information contained in this handbook was obtained from materials producers,industry,reports on Government sponsored research,the open literature,and by contact with research laboratories and those who participate in the MIL-HDBK-17 coordination activity. 7.All information and data contained in this handbook have been coordinated with industry and the U.S. Army,Navy,Air Force,NASA,and Federal Aviation Administration prior to publication. 8.Copies of this document and revisions thereto may be obtained from the Document Automation and Production Service (DAPS),Bldg.4D (DODSSP/ASSIST),700 Robbins Avenue,Philadelphia,PA 19111-5094. 9.Beneficial comments(recommendations,additions,deletions)and any pertinent data which may be of use in improving this document should be addressed to:U.S.Army Research Laboratory,Weapons and Materials Research Directorate,Attn:AMSRL-WM-MA,Aberdeen Proving Ground,MD 21005- 5069,by using the Standardization Document Improvement Proposal(DD Form 1426)appearing at the end of this document or by letter. 心
MIL-HDBK-17-3F Volume 3, Foreword / Table of Contents ii FOREWORD 1. This Composite Materials Handbook Series, MIL-HDBK-17, are approved for use by all Departments and Agencies of the Department of Defense. 2. This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply. This mandate is a DoD requirement only; it is not applicable to the Federal Aviation Administration (FAA) or other government agencies. 3. Every effort has been made to reflect the latest information on polymer (organic), metal, and ceramic composites. The handbook is continually reviewed and revised to ensure its completeness and currentness. Documentation for the secretariat should be directed to: Materials Sciences Corporation, MIL-HDBK-17 Secretariat, 500 Office Center Drive, Suite 250, Fort Washington, PA 19034. 4. MIL-HDBK-17 provides guidelines and material properties for polymer (organic), metal, and ceramic matrix composite materials. The first three volumes of this handbook currently focus on, but are not limited to, polymeric composites intended for aircraft and aerospace vehicles. Metal matrix composites (MMC) and ceramic matrix composites (CMC), including carbon-carbon composites (C-C) are covered in Volume 4 and Volume 5 , respectively. 5. This standardization handbook has been developed and is being maintained as a joint effort of the Department of Defense and the Federal Aviation Administration. 6. The information contained in this handbook was obtained from materials producers, industry, reports on Government sponsored research, the open literature, and by contact with research laboratories and those who participate in the MIL-HDBK-17 coordination activity. 7. All information and data contained in this handbook have been coordinated with industry and the U.S. Army, Navy, Air Force, NASA, and Federal Aviation Administration prior to publication. 8. Copies of this document and revisions thereto may be obtained from the Document Automation and Production Service (DAPS), Bldg. 4D (DODSSP/ASSIST), 700 Robbins Avenue, Philadelphia, PA 19111-5094. 9. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: U.S. Army Research Laboratory, Weapons and Materials Research Directorate, Attn: AMSRL-WM-MA, Aberdeen Proving Ground, MD 21005- 5069, by using the Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter
MIL-HDBK-17-3F Volume 3,Foreword Table of Contents SUMMARY OF CHANGES Chapter Section Title Change type All All The entire volume has been reorganized revision 1 1.1 Introduction revision 2 2.4.1.1. Carbon Fibers new 2 2.4.1.8 Ultrahigh Molecular Weight Polyethylene new 2 2.7.1 Automated Tape Placement new 2 2.7.2 Fiber Placement/Automated Tow Placement new 2 2.7.8 Adhesive Bonding revision 2 2.8.7 Resin Transfer molding revision 3 3.4 Statistical Process Control revision 3.5 Managing Change in Materials and Processes new 4 All sections Design and Analysis(Rev E), Now is Chapter 5.with new and Building Block Approach for Composite Structures revised material (Rev F) 5 All sections Structural Behavior of Joints(Rev E) Now is Chapter 6,with new and Design and Analysis(Rev F) revised material 6 All sections Structural Reliability (Rev E) Now is Chapter 9,with new and Structural Behavior of Joints(Rev F) revised material 7 All sections Thick Section Composites(Rev E) Now is Chapter 10,with new Damage Resistance,Durability,and Damage and revised material Tolerance(Rev F) 8 All sections Supportability revised 9 All sections Lessons Learned (Rev E) Now is Chapter 12,with new Structural Reliability (Rev F) and revised material 10 All sections Thick Section Composites Refer to Chap 7 entry 11 All sections Environmental Management new 12 All sections Lessons Learned Refer to Chap 9 entry xvii
MIL-HDBK-17-3F Volume 3, Foreword / Table of Contents xvii SUMMARY OF CHANGES Chapter Section Title Change type All All The entire volume has been reorganized revision 1 1.1 Introduction revision 2 2.4.1.1. Carbon Fibers new 2 2.4.1.8 Ultrahigh Molecular Weight Polyethylene new 2 2.7.1 Automated Tape Placement new 2 2.7.2 Fiber Placement/Automated Tow Placement new 2 2.7.8 Adhesive Bonding revision 2 2.8.7 Resin Transfer molding revision 3 3.4 Statistical Process Control revision 3.5 Managing Change in Materials and Processes new 4 All sections Design and Analysis (Rev E), Building Block Approach for Composite Structures (Rev F) Now is Chapter 5, with new and revised material 5 All sections Structural Behavior of Joints (Rev E) Design and Analysis (Rev F) Now is Chapter 6, with new and revised material 6 All sections Structural Reliability (Rev E) Structural Behavior of Joints (Rev F) Now is Chapter 9, with new and revised material 7 All sections Thick Section Composites(Rev E) Damage Resistance, Durability, and Damage Tolerance (Rev F) Now is Chapter 10, with new and revised material 8 All sections Supportability revised 9 All sections Lessons Learned (Rev E) Structural Reliability (Rev F) Now is Chapter 12, with new and revised material 10 All sections Thick Section Composites Refer to Chap 7 entry 11 All sections Environmental Management new 12 All sections Lessons Learned Refer to Chap 9 entry
