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طراحی وسایل نقلیه فضایی، ویرایش دوم

Space Vehicle Design, Second Edition (AIAA Education)

جلد کتاب طراحی وسایل نقلیه فضایی، ویرایش دوم

معرفی کتاب «طراحی وسایل نقلیه فضایی، ویرایش دوم» (با عنوان لاتین Space Vehicle Design, Second Edition (AIAA Education)) نوشتهٔ Sylvain Kerkour و Michael D Griffin, James R French, M Griffin and J French، منتشرشده توسط نشر AIAA (American Institute of Aeronautics & Astronautics) در سال 2004. این کتاب در فرمت pdf، زبان انگلیسی ارائه شده است.

I used this book in a space vehicle design class. If you intend to use this text to gain a broad understanding of the basic design considerations for space vehicles, I believe you will be satisfied. If, however, you would like to go into depth regarding rocket propulsion, orbital mechanics, structural/vibration analysis, reentry, etc. look for a text which is devoted to those topics. This text does cover such topics as well as others but is lacking in detail. There are some good examples throughout each chapter and problems at the end of each chapter. Cover Copyright Title Foreword to the Previous Edition Table of Contents Preface Preface to the Previous Edition Chapter 1 Introduction 1.1 Introduction 1.2 Systems Engineering Process 1.3 Requirements and Tradeoffs Bibliography Chapter 2 Mission Design 2.1 Introduction 2.2 Low Earth Orbit 2.3 Medium-Altitude Earth Orbit 2.4 Geosynchronous Earth Orbit 2.5 Lunar and Deep Space Missions 2.6 Advanced Mission Concepts Bibliography Chapter 3 Spacecraft Environment 3.1 Introduction 3.2 Earth Environment 3.3 Launch Environment 3.4 Atmospheric Environment 3.5 Space and Upper Atmosphere Environment References Problems Chapter 4 Astrodynamics 4.1 Introduction 4.2 Fundamentals of Orbital Mechanics 4.3 Non-Keplerian Motion 4.4 Basic Orbital Maneuvers 4.5 Interplanetary Transfer 4.6 Perturbation Methods 4.7 Orbital Rendezvous References Problems Chapter 5 Propulsion 5.1 Rocket Propulsion Fundamentals 5.2 Ascent Flight Mechanics 5.3 Launch Vehicle Selection References Problems Chapter 6 Atmospheric Entry 6.1 Introduction 6.2 Fundamentals of Entry Flight Mechanics 6.3 Fundamentals of Entry Heating 6.4 Entry Vehicle Designs 6.5 Aeroassisted Orbit Transfer References Bibliography Problems Chapter 7 Attitude Determination and Control 7.1 Introduction 7.2 Basic Concepts and Terminology 7.3 Review of Rotational Dynamics 7.4 Rigid Body Dynamics 7.5 Space Vehicle Disturbance Torques 7.6 Passive Attitude Control 7.7 Active Control 7.8 Attitude Determination 7.9 System Design Considerations References Problems Chapter 8 Configuration and Structural Design 8.1 Introduction 8.2 Design Drivers 8.3 Spacecraft Design Concepts 8.4 Mass Properties 8.5 Structural Loads 8.6 Large Structures 8.7 Materials References Chapter 9 Thermal Control 9.1 Introduction 9.2 Spacecraft Thermal Environment 9.3 Thermal Control Methods 9.4 Heat Transfer Mechanisms 9.5 Spacecraft Thermal Modeling and Analysis References Problems Chapter 10 Power Systems 10.1 Introduction 10.2 Power System Functions 10.3 Power System Evolution 10.4 Power System Design Drivers 10.5 Power System Elements 10.6 Design Practice 10.7 Batteries 10.8 Primary Power Source 10.9 Solar Arrays 10.10 Radioisotope Thermoelectric Generators 10.11 Fuel Cells 10.12 Power Conditioning and Control 10.13 Future Concepts References Problems Chapter 11 Telecommunications 11.1 Introduction 11.2 Command Subsystem 11.3 Hardware Redundancy 11.4 Autonomy 11.5 Command Subsystem Elements 11.6 Radio Frequency Elements 11.7 Spacecraft Tracking References Problems Chapter 12 Reliability Analysis 12.1 Introduction 12.2 Review of Probability Theory 12.3 Random Variables 12.4 Special Probability Distributions 12.5 System Reliability 12.6 Statistical Inference 12.7 Design Considerations References Problems Appendix A: Random Processes Appendix B: Tables Bibliography Index

Winner of the Summerfield Book Award!

The second edition continues to fulfill the book's original goal—that of linking and integrating the many disciplines relevant to the field of space systems engineering in a way that is impossible when they are considered separately, or even in one text that is the product of many authors. The text starts with an overall description of the basic mission considerations for spacecraft design, including space environment, astrodynamics, and atmospheric reentry. Then the various subsystems are discussed, and in each case, both the theoretical background and the current engineering practice are fully explained. Some material has been updated to make the treatment consistent with current experience and practice in the field. At the same time, there is much that remains relevant from what are now the earlier decades of the space program. Nothing of real value has been omitted merely on the grounds that it is old. This edition contains a new chapter on reliability analysis, much new technical material in other sections, and many homework problems. The book provides the space systems engineer with the tools to evaluate the overall impact of candidate design concepts on the various component subsystems and the integrated system leading to the final design selection.

The second edition of this text continues to fulfil the book's original goal in linking and integrating many disciplines relevant to the field of space systems engineering. It contains an additional chapter on reliability analysis, new technical material and numerous homework problems.
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