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0 (hodnocen0 x )

EB

ONLINE

1st ed.

Reston : American Institute of Aeronautics & Astronautics, 2018

1 online resource (845 pages)

ISBN 9781624104893 (electronic bk.)

ISBN 9781624104886

Progress in Astronautics and Aeronautics Ser.

Print version: Bhat, Biliyar N. Aerospace Materials and Applications Reston : American Institute of Aeronautics & Astronautics,c2018 ISBN 9781624104886

Cover -- Half Title -- Title Page -- Copyright Page -- Table of Contents -- Preface -- Chapter 1: Introduction -- Chapter 2: Aerospace Materials Characteristics -- 2.1 INTRODUCTION -- 2.2 ALUMINUM ALLOYS -- 2.3 TITANIUM ALLOYS -- 2.4 STEELS -- 2.5 SUPERALLOYS -- 2.6 COPPER ALLOYS -- 2.7 DAMAGE TOLERANCE CONSIDERATIONS FOR METALLIC MATERIALS -- 2.8 HYDROGEN EMBRITTLEMENT IN METALLIC MATERIALS -- 2.9 MATERIAL BEHAVIOR IN OXYGEN-RICH ENVIRONMENTS -- 2.10 POLYMERS AND COMPOSITES -- 2.11 POLYMER MATRIX COMPOSITES IN AEROSPACE STRUCTURES -- 2.12 AEROSPACE CERAMIC MATERIALS -- ACKNOWLEDGEMENTS -- REFERENCES -- Chapter 3: Materials Selection for Aerospace Systems -- 3.1 INTRODUCTION -- 3.2 SYSTEMATIC APPROACH TO MATERIALS SELECTION -- 3.3 ADVANCED SELECTION -- 3.4 DATA ISSUES -- 3.5 SUMMARY -- REFERENCES -- Chapter 4: Advanced Nanoengineered Materials -- 4.1 INTRODUCTION -- 4.2 NANOENGINEERED STRUCTURAL MATERIALS -- 4.3 NANOENGINEERED MULTIFUNCTIONAL MATERIALS -- 4.4 PROCESSING AND MANUFACTURING -- 4.5 MODELING OF NANOMATERIALS: MULTISCALE AND MULTITECHNIQUE -- 4.6 FUTURE TRENDS -- ACKNOWLEDGMENTS -- REFERENCES -- Chapter 5: Subsonic Aircraft Materials Development -- 5.1 INTRODUCTION -- 5.2 SUBSONIC AND SUPERSONIC FIXED WING AIRCRAFT -- 5.3 ROTORCRAFT -- 5.4 ENABLING MATERIALS, STRUCTURES, AND MANUFACTURING PROCESSES -- 5.5 CLOSING COMMENTS -- ACKNOWLEDGEMENTS -- REFERENCES -- Chapter 6: Materials for Spacecraft -- 6.1 INTRODUCTION -- 6.2 SPACE ENVIRONMENT -- 6.3 SPACECRAFT DESIGN AND MATERIALS REQUIREMENTS -- 6.4 FLAMMABILITY, TOXICITY, AND OFFGASSING CONSIDERATIONS -- 6.5 STRUCTURAL MATERIALS -- 6.6 THERMAL CONTROL MATERIALS -- 6.7 THERMAL PROTECTION MATERIALS -- 6.8 RADIATION SHIELDING -- 6.9 METEOROID/ORBITAL DEBRIS SHIELDING -- 6.10 OPTICAL MATERIALS -- 6.11 SOLAR ARRAY MATERIALS -- 6.12 LUBRICANTS -- 6.13 SEAL MATERIALS -- 6.14 ADHESIVES.

12.8 LINES AND DUCTS -- 12.9 SUMMARY -- REFERENCES -- Chapter 13: Advanced Materials for In-Space Propulsion -- 13.1 INTRODUCTION -- 13.2 CHEMICAL PROPULSION (LIQUID STORABLE AND LIQUID CRYOGENIC) -- 13.3 GRIDDED ION THRUSTERS -- 13.4 HALL PROPULSION SYSTEMS -- 13.5 SOLAR THERMAL PROPULSION -- 13.6 NUCLEAR THERMAL PROPULSION -- 13.7 SOLAR SAIL PROPULSION -- 13.8 TETHER PROPULSION -- 13.9 ADVANCED PROPULSION TECHNOLOGIES -- 13.10 SUMMARY -- REFERENCES -- Chapter 14: Materials for Power Systems in Space Exploration -- 14.1 INTRODUCTION -- 14.2 SOLAR -- 14.3 FUEL CELLS -- 14.4 BATTERIES -- 14.5 RADIOISOTOPE POWER SYSTEMS -- 14.6 FISSION POWER FOR SPACE -- 14.7 CONCLUDING REMARKS -- REFERENCES -- Index -- Supporting Materials.

6.15 LESSONS LEARNED -- 6.16 CONCLUDING REMARKS -- ACKNOWLEDGMENTS -- REFERENCES -- Chapter 7: Materials for Launch Vehicle Structures -- 7.1 INTRODUCTION -- 7.2 LAUNCH VEHICLE STRUCTURES -- 7.3 BASIC MATERIAL CHARACTERISTICS -- 7.4 STRUCTURAL DESIGN AND REQUIREMENTS -- 7.5 PRESSURIZED STRUCTURE -- 7.6 FEEDLINES, SMALL LINES, AND PRESSURE VESSELS -- 7.7 UNPRESSURIZED STRUCTURE -- 7.8 THERMAL PROTECTION AND INSULATION -- 7.9 MANUFACTURING CONSIDERATIONS -- 7.10 SUMMARY, TRENDS, AND OUTLOOK -- REFERENCES -- Chapter 8: Materials for Exploration Systems -- 8.1 INTRODUCTION -- 8.2 DEVELOPMENT OF A TECHNICAL BASIS FOR MATERIALS PROCESSING IN SPACE -- 8.3 DEVELOPMENT OF AN ECONOMIC BASIS FOR MATERIALS PROCESSING IN SPACE: IN SITU PROPELLANT PRODUCTION -- 8.4 SUMMARY AND CONCLUSIONS -- REFERENCES -- Chapter 9: Thermal Protection Systems and Hot Structures for Hypersonic Vehicles -- 9.1 INTRODUCTION -- 9.2 BACKGROUND -- 9.3 TPS AND HOT STRUCTURE COMPONENTS -- 9.4 KEY TECHNICAL CHALLENGES -- 9.5 CONCLUDING REMARKS -- ACKNOWLEDGMENTS -- REFERENCES -- Chapter 10: Aero Engine Materials -- 10.1 INTRODUCTION -- 10.2 BRIEF HISTORICAL PERSPECTIVE ON AIRCRAFT ENGINE EVOLUTION -- 10.3 EVOLUTION OF JET ENGINE MATERIALS -- 10.4 MATERIALS PROCESSING -- 10.5 TRENDS AND OUTLOOK -- 10.6 SUMMARY -- BIBLIOGRAPHY -- Chapter 11: Materials for Solid Rocket Engines -- 11.1 INTRODUCTION -- 11.2 SOLID ROCKET COMPONENTS -- 11.3 MOTOR CASES -- 11.4 INSULATION MATERIALS -- 11.5 LINER AND INHIBITOR -- 11.6 NOZZLE -- 11.7 IGNITERS -- 11.8 HYBRID ROCKET PROPULSION SYSTEMS -- 11.9 SUMMARY, TRENDS, AND OUTLOOK -- BIBLIOGRAPHY -- Chapter 12: Materials for Liquid Propulsion Systems -- 12.1 INTRODUCTION -- 12.2 LIQUID ROCKET ENGINES -- 12.3 GENERAL DESIGN CONSIDERATIONS FOR MATERIALS SELECTION -- 12.4 MATERIALS -- 12.5 THRUST CHAMBER MATERIALS -- 12.6 TURBOPUMP MATERIALS -- 12.7 VALVES.

Aerospace Materials and Applications addresses materials selection and use in aircraft, spacecraft, launch vehicles, and propulsion systems and power systems. Advances in aerospace systems are strongly dependent on advances in materials and processing technologies. In the past hundred years of powered flight aircraft structures have evolved around advances in materials that are lighter and stronger. Aircraft propulsion systems are constantly striving to become more fuel efficient via reductions in mass and improved capability for materials to operate at higher temperatures for longer periods. Gas turbine engines that power modern aircraft are being designed to run at higher pressures and temperatures to generate more thrust per pound of engine mass. Similar considerations apply to rocket engines where the power densities are much higher. Spacecraft are designed to operate in the harsh radiation environments of outer space. In-space propulsion and power systems are key components of spacecraft and advanced materials enable these systems. Hence it is important for aerospace systems designers to have a good understanding of how specific materials will perform in their systems. Aerospace Materials and Applications clearly shows the preferred approach to selecting materials given the unique requirements for design and construction of aerospace systems..

001905865

express

(Au-PeEL)EBL29191765

(MiAaPQ)EBC29191765

(OCoLC)1112606278