Spacecraft Structures and Mechanisms: From Concept to Launch

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9780792334767: Spacecraft Structures and Mechanisms: From Concept to Launch

Spacecraft Structures and Mechanisms describes the integral process of developing cost-effective, reliable structures and mechanical products for space programs. Processes are defined, methods are described and examples are given. It has been written by 24 engineers in the space industry, who cover the themes of (1) ensuring a successful mission, and (2) reducing total cost through good designs and intelligent risk management. Topics include: Introduction and requirements (development process, requirements documentation, requirements definition, space mission environments); Analysis (statics, dynamics and load analysis, fatigue and fracture mechanics, mechanics of materials, strength analysis, heat transfer and thermal effects); Verification and quality assurance (verification planning, structural, mechanical and environmental testing, quality assurance and configuration control, compliance documentation, structural reliability analysis, verification criteria - factors of safety, margins of safety, fracture control, test options); Design (spacecraft configuration development, finite element analysis, mechanism development, designing for producibility, structural design, materials, designing to control loads, load cycles, sensitivity analysis); Final verification (model correlation, risk management, launch readiness reviews). For system engineers, mechanical designers, stress analysts, dynamics and load analysts, technical leads, program managers.

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Contenuti:

Preface. Part I: Introduction. 1. Developing Spacecraft Structures and Mechanisms. Part II: Requirements. 2. Developing Mechanical Requirements and Conceptual Designs. 3. Space Mission Environments. P art III: Analysis. 4. Structural Mechanics. 5. Loads Analysis for Single-Degree-of-Freedom Systems. 6. Mechanics of Materials. 7. Flexible-Body Dynamics. 8. Strength Analysis. 9. Structural Life Analysis. 10. Thermal Effects. Part IV: Verification and Quality Assurance. 11. Developing Confidence in Mechanical Designs and Products. 12. Verification Criteria. 13. Ensuring Quality. Part V: Design. 14. Configuring a Spacecraft. 15. Conceptual Design of Structures. 16. Idealizing and Modeling Structures. 17. Controlling Structural Responses. 18. Design Loads Cycles. 19. Developing Mechanisms. Part VI: Final Verification. 20. Designing for Producibility. 21. Final Verification. Appendixes: A. Units and Conversion Factors. B. Effective Verification Documentation. C. Structural Reliability Analysis. D. Standard Normal Probability Table. E. Preparing for and Documenting Tests. F. Spacecraft Integration and Test. G. Estimating Structural Damping. Index.

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1.

Wiley Larson
ISBN 10: 0792334760 ISBN 13: 9780792334767
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Descrizione libro Condizione libro: New. This item is Print on Demand - Depending on your location, this item may ship from the US or UK. Codice libro della libreria POD_9780792334767

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Wiley Larson
Editore: Kluwer Academic Publishers, United States (1995)
ISBN 10: 0792334760 ISBN 13: 9780792334767
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Descrizione libro Kluwer Academic Publishers, United States, 1995. Hardback. Condizione libro: New. 1995.. 241 x 163 mm. Language: English . Brand New Book. Spacecraft Structures and Mechanisms describes the integral process of developing cost-effective, reliable structures and mechanical products for space programs. Processes are defined, methods are described and examples are given. It has been written by 24 engineers in the space industry, who cover the themes of (1) ensuring a successful mission, and (2) reducing total cost through good designs and intelligent risk management. Topics include: Introduction and requirements (development process, requirements documentation, requirements definition, space mission environments); Analysis (statics, dynamics and load analysis, fatigue and fracture mechanics, mechanics of materials, strength analysis, heat transfer and thermal effects); Verification and quality assurance (verification planning, structural, mechanical and environmental testing, quality assurance and configuration control, compliance documentation, structural reliability analysis, verification criteria - factors of safety, margins of safety, fracture control, test options); Design (spacecraft configuration development, finite element analysis, mechanism development, designing for producibility, structural design, materials, designing to control loads, load cycles, sensitivity analysis); Final verification (model correlation, risk management, launch readiness reviews). For system engineers, mechanical designers, stress analysts, dynamics and load analysts, technical leads, program managers. Codice libro della libreria LIB9780792334767

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Wiley Larson
Editore: Kluwer Academic Publishers, United States (1995)
ISBN 10: 0792334760 ISBN 13: 9780792334767
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Descrizione libro Kluwer Academic Publishers, United States, 1995. Hardback. Condizione libro: New. 1995.. 241 x 163 mm. Language: English . Brand New Book. Spacecraft Structures and Mechanisms describes the integral process of developing cost-effective, reliable structures and mechanical products for space programs. Processes are defined, methods are described and examples are given. It has been written by 24 engineers in the space industry, who cover the themes of (1) ensuring a successful mission, and (2) reducing total cost through good designs and intelligent risk management. Topics include: Introduction and requirements (development process, requirements documentation, requirements definition, space mission environments); Analysis (statics, dynamics and load analysis, fatigue and fracture mechanics, mechanics of materials, strength analysis, heat transfer and thermal effects); Verification and quality assurance (verification planning, structural, mechanical and environmental testing, quality assurance and configuration control, compliance documentation, structural reliability analysis, verification criteria - factors of safety, margins of safety, fracture control, test options); Design (spacecraft configuration development, finite element analysis, mechanism development, designing for producibility, structural design, materials, designing to control loads, load cycles, sensitivity analysis); Final verification (model correlation, risk management, launch readiness reviews). For system engineers, mechanical designers, stress analysts, dynamics and load analysts, technical leads, program managers. Codice libro della libreria LIB9780792334767

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Sarafin, Thomas P. (EDT)/ Larson, Wiley J. (EDT)
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Descrizione libro Kluwer Academic Publishers. hardback. Condizione libro: New. Codice libro della libreria 9780792334767

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THOMAS P. SARAFIN
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Descrizione libro Springer, 1995. Hardback. Condizione libro: NEW. 9780792334767 This listing is a new book, a title currently in-print which we order directly and immediately from the publisher. Codice libro della libreria HTANDREE0280247

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Thomas P. Sarafin
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Descrizione libro Kluwer Academic Publishers, 1995. HRD. Condizione libro: New. New Book. Delivered from our US warehouse in 10 to 14 business days. THIS BOOK IS PRINTED ON DEMAND.Established seller since 2000. Codice libro della libreria IP-9780792334767

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Sarafin, Thomas P.
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Descrizione libro Springer, 2016. Paperback. Condizione libro: New. PRINT ON DEMAND Book; New; Publication Year 2016; Not Signed; Fast Shipping from the UK. No. book. Codice libro della libreria ria9780792334767_lsuk

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Thomas P. Sarafin
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Descrizione libro Kluwer Academic Publishers, 1995. HRD. Condizione libro: New. New Book.Shipped from US within 10 to 14 business days.THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Codice libro della libreria IP-9780792334767

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Thomas P. Sarafin
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Descrizione libro Springer Mai 1995, 1995. Buch. Condizione libro: Neu. 235x155x52 mm. Neuware - Spacecraft Structures and Mechanisms describes the integral process of developing cost-effective, reliable structures and mechanical products for space programs. Processes are defined, methods are described and examples are given. It has been written by 24 engineers in the space industry, who cover the themes of (1) ensuring a successful mission, and (2) reducing total cost through good designs and intelligent risk management. Topics include: Introduction and requirements (development process, requirements documentation, requirements definition, space mission environments); Analysis (statics, dynamics and load analysis, fatigue and fracture mechanics, mechanics of materials, strength analysis, heat transfer and thermal effects); Verification and quality assurance (verification planning, structural, mechanical and environmental testing, quality assurance and configuration control, compliance documentation, structural reliability analysis, verification criteria - factors of safety, margins of safety, fracture control, test options); Design (spacecraft configuration development, finite element analysis, mechanism development, designing for producibility, structural design, materials, designing to control loads, load cycles, sensitivity analysis); Final verification (model correlation, risk management, launch readiness reviews). For system engineers, mechanical designers, stress analysts, dynamics and load analysts, technical leads, program managers. 868 pp. Englisch. Codice libro della libreria 9780792334767

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Thomas P. Sarafin
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ISBN 10: 0792334760 ISBN 13: 9780792334767
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Descrizione libro Springer Mai 1995, 1995. Buch. Condizione libro: Neu. 235x155x52 mm. Neuware - Spacecraft Structures and Mechanisms describes the integral process of developing cost-effective, reliable structures and mechanical products for space programs. Processes are defined, methods are described and examples are given. It has been written by 24 engineers in the space industry, who cover the themes of (1) ensuring a successful mission, and (2) reducing total cost through good designs and intelligent risk management. Topics include: Introduction and requirements (development process, requirements documentation, requirements definition, space mission environments); Analysis (statics, dynamics and load analysis, fatigue and fracture mechanics, mechanics of materials, strength analysis, heat transfer and thermal effects); Verification and quality assurance (verification planning, structural, mechanical and environmental testing, quality assurance and configuration control, compliance documentation, structural reliability analysis, verification criteria - factors of safety, margins of safety, fracture control, test options); Design (spacecraft configuration development, finite element analysis, mechanism development, designing for producibility, structural design, materials, designing to control loads, load cycles, sensitivity analysis); Final verification (model correlation, risk management, launch readiness reviews). For system engineers, mechanical designers, stress analysts, dynamics and load analysts, technical leads, program managers. 868 pp. Englisch. Codice libro della libreria 9780792334767

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