1 INTRODUCTION
- 1.1 Payloads and Missions
- 1.2 A System View of Spacecraft
- 1.3 The Future
2 THE SPACECRAFT ENVIRONMENT AND ITS EFFECT ON DESIGN
- 2.1 Introduction
- 2.2 Pre-Operational Spacecraft Environments
- 2.3 Operational Spacecraft Environments
- 2.4 Environmental Effects on Design
3 DYNAMICS OF SPACECRAFT
- 3.1 Introduction
- 3.2 Trajectory Dynamics
- 3.3 General Attitude Dynamics
- 3.4 Attitude Motion of Specific Types of Spacecraft
- 3.5 Oscillatory Modes
- 3.6 In Conclusion
- Appendix: The Inertia Matrix
4 CELESTIAL MECHANICS
- 4.1 Introduction
- 4.2 The Two-body Problem—Particle Dynamics
- 4.3 Specifying the Orbit
- 4.4 Orbit Perturbations
- 4.5 Restricted Three-body Problem
5 MISSION ANALYSIS
- 5.1 Introduction
- 5.2 Keplerian Orbit Transfers
- 5.3 Mission Analysis
- 5.4 Polar LEO/Remote-Sensing Satellites
- 5.5 Satellite Constellations
- 5.6 Geostationary Earth Orbits (GEO)
- 5.7 Highly Elliptic Orbits
- 5.8 Interplanetary Missions
6 PROPULSION SYSTEMS
- 6.1 Systems Classification
- 6.2 Chemical Rockets
- 6.3 Spacecraft Propulsion
- 6.4 Electric Propulsion
7 LAUNCH VEHICLES
- 7.1 Introduction
- 7.2 Basic Launch Vehicle Performance and Operation
- 7.3 Spacecraft Launch Phases and Mission Planning
- 7.4 The Ariane 5 Launch Vehicle
- 7.5 US Crewed Launch Systems
- 7.6 Small Launchers and Reusable Sub-Orbital Vehicles
- 7.7 Re-Entry into Earth’s Atmosphere
- 7.8 Specific Launch Costs and Reliability
8 SPACECRAFT STRUCTURES
- 8.1 Introduction
- 8.2 Design Requirements
- 8.3 Material Selection
- 8.4 Analysis
- 8.5 Design Verification
- 8.6 Impact Protection
- 8.7 Configuration Examples
- 8.8 The Future of Space Structures
9 ATTITUDE CONTROL
- 9.1 Introduction
- 9.2 ACS Overview
- 9.3 The Spacecraft Attitude Response
- 9.4 Torques and Torquers
- 9.5 Attitude Measurement
- 9.6 ACS Computation
10 ELECTRICAL POWER SYSTEMS
- 10.1 Introduction
- 10.2 Power System Elements
- 10.3 Primary Power Systems
- 10.4 Secondary Power Systems: Batteries
- 10.5 Power Management, Distribution and Control
- 10.6 Power Budget
11 THERMAL CONTROL OF SPACECRAFT
- 11.1 Introduction
- 11.2 The Thermal Environment
- 11.3 Thermal Balance
- 11.4 Thermal Analysis
- 11.5 Thermal Design
- 11.6 Thermal Technology
- 11.7 Thermal Design Verification
- 11.8 Example of Satellite Thermal Design—XMM/Newton
12 TELECOMMUNICATIONS
- 12.1 Introduction
- 12.2 Techniques of Radio Communications
- 12.3 The Communications Payload
- 12.4 Conclusion
13 TELEMETRY, COMMAND, DATA HANDLING AND PROCESSING
- 13.1 Introduction
- 13.2 System Architecture
- 13.3 Telemetry Data Formatting
- 13.4 Telecommand
- 13.5 Communication Techniques and Protocols
- 13.6 On-Board Data Handling (OBDH) and Processing
- 13.7 Technology
- 13.8 Tools and Controlling Documents
14 GROUND SEGMENT
- 14.1 Introduction
- 14.2 The Ground Station
- 14.3 Flight Dynamics
- 14.4 The Ground Data System
- 14.5 The Flight Operations System
15 SPACECRAFT MECHANISMS
- 15.1 Introduction
- 15.2 One-Shot Devices
- 15.3 Continuously and Intermittently Operating Devices
- 15.4 Components
- 15.5 Materials
- 15.6 Tribology
- 15.7 Testing and Verification
- 15.8 Conclusion
16 SPACECRAFT ELECTROMAGNETIC COMPATIBILITY ENGINEERING
- 16.1 Introduction
- 16.2 Examples of EMC Problems
- 16.3 EMC Specifications
- 16.4 Electromagnetic Compatibility—Terms and Definitions
- 16.5 EMC Fundamentals
- 16.6 The Systems Approach to EMC
- 16.7 EMC Categories
- 16.8 Electrostatic Discharge
- 16.9 Spacecraft Grounding Schemes
- 16.10 Major Causes of Spacecraft EMC Problems
- 16.11 Analysis Methods for Spacecraft EMC Engineering
17 ASSEMBLY, INTEGRATION AND VERIFICATION
- 17.1 Introduction
- 17.2 Some Definitions
- 17.3 The Verification Plan
- 17.4 Relationship between Analysis and Test
- 17.5 The AIV Plan
- 17.6 Testing: General
- 17.7 Test Types
- 17.8 Model Philosophy
- 17.9 Build Standards and Applications
- 17.10 Ground Support Equipment
- 17.11 Checkpoints in the AIV Programme
- 17.12 Verification Closeout
- 17.13 Launch Preparation
- 17.14 Conclusion
18 SMALL SATELLITE ENGINEERING AND APPLICATIONS
- 18.1 Introduction
- 18.2 Small Satellite Design Philosophy
- 18.3 Small Satellite System Design
- 18.4 COTS Components in the Space Environment
- 18.5 Microsatellite Platforms
- 18.6 Minisatellite Platforms
- 18.7 Nanosatellite Platforms
- 18.8 Affordable Launches for Small Satellites
- 18.9 In-Orbit Operations
- 18.10 Small Satellite Applications
- 18.11 Picosatellites and Recent Advances in Miniaturization
- 18.12 Conclusion
19 PRODUCT ASSURANCE
- 19.1 Introduction
- 19.2 Product Assurance in a Project
- 19.3 Reliability/Dependability
- 19.4 Parts
- 19.5 Materials and Processes
- 19.6 Product Assurance in Manufacturing, AI&V
- 19.7 Safety
- 19.8 Product Assurance in Operations
- 19.9 Software Product Assurance
- 19.10 PA in Technology Developments
- 19.11 The Assurance Message
20 SPACECRAFT SYSTEM ENGINEERING
- 20.1 Introduction
- 20.2 System Engineering
- 20.3 Concurrent Engineering
- 20.4 A Case Study: Cryosat
- 20.5 Conclusion
Index
This fourth edition of the bestselling Spacecraft Systems Engineering title provides the reader with comprehensive coverage of the design of spacecraft and the implementation of space missions, across a wide spectrum of space applications and space science. The text has been thoroughly revised and updated, with each chapter authored by a recognized expert in the field. Three chapters – Ground Segment, Product Assurance and Spacecraft System Engineering – have been rewritten, and the topic of Assembly, Integration and Verification has been introduced as a new chapter, filling a gap in previous editions.
This edition addresses ‘front-end system-level issues’ such as environment, mission analysis and system engineering, but also progresses to a detailed examination of subsystem elements which represents the core of spacecraft design. This includes mechanical, electrical and thermal aspects, as well as propulsion and control. This quantitative treatment is supplemented by an emphasis on the interactions between elements, which deeply influences the process of spacecraft design.
Adopted on courses worldwide, Spacecraft Systems Engineering is already widely respected by students, researchers and practising engineers in the space engineering sector. It provides a valuable resource for practitioners in a wide spectrum of disciplines, including system and subsystem engineers, spacecraft equipment designers, spacecraft operators, space scientists and those involved in related sectors such as space insurance.
In summary, this is an outstanding resource for aerospace engineering students, and all those involved in the technical aspects of design and engineering in the space sector.
Key Features
- Updated edition of this bestelling & well-established introductory guide to the engineering of spacecraft for students and engineers alike.
- Provides balanced and comprehensive coverage of the different and diverse areas of engineering required in the design and implementation of spacecraft and space missions.
- Includes major revisions to the chapters on launch vehicles, structures, ground stations and mechanisms, and a new chapter on Assembly, Integration and Test.
- Unique in its approach that is rooted in and reflects the new developments in European space technology, which continues to mature at a rapid speed.
New to this edition
- With emphasis on recent developments in space activities, all chapters have been rewritten with major revisions to the chapters on launch vehicles, structures, ground stations and mechanisms, and a brand new chapter on Assembly, Integration and Test.
Book Details
- Hardcover: 724 pages
- Publisher: Wiley; 4 edition (September 27, 2011)
- Language: English
- ISBN-10: 047075012X
- ISBN-13: 978-0470750124
- Product Dimensions: 6.9 x 1.7 x 9.8 inches
- List Price: $75.00