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Spacecraft systems engineering / edited by Peter Fortescue, John Stark, Graham Swinerd.
- Format:
- Book
- Language:
- English
- Subjects (All):
- Space vehicles--Design and construction.
- Space vehicles.
- Astronautics--Systems engineering.
- Astronautics.
- Physical Description:
- xxvi, 678 pages : illustrations ; 25 cm
- Edition:
- Third edition.
- Place of Publication:
- New York : J. Wiley, [2003]
- Summary:
- Following on from the hugely successful previous editions, the third edition of Spacecraft Systems Engineering incorporates the most recent technological advances in spacecraft and satellite engineering. With emphasis on recent developments in space activities, this new edition has been completely revised. Every chapter has been updated and rewritten by an expert engineer in the field, with emphasis on the bus rather than the payload. Encompassing the fundamentals of spacecraft engineering, the book begins with front-end system-level issues, such as environment, mission analysis and system engineering, and progresses to a detailed treatment of subsystem elements which represent the core of spacecraft design -- mechanical, electrical, propulsion, thermal, control etc. This quantitative treatment is supplemented by an appreciation of the interactions between the elements, which deeply influence the process of spacecraft systems design. In summary, this is an outstanding textbook for aerospace engineering and design students, and offers essential reading for spacecraft engineers, designers and research scientists. The comprehensive approach provides an invaluable resource to spacecraft manufacturers and agencies across the world.
- Contents:
- 1.1 Payloads and Missions 2
- 1.2 A System View of Spacecraft 4
- 1.3 The Future 8
- 2 The Spacecraft Environment and its Effect on Design / John P. W. Stark
- 2.2 Pre-Operational Spacecraft Environments 11
- 2.3 Operational Spacecraft Environments 17
- 2.4 Environmental Effects on Design 39
- 3 Dynamics of Spacecraft / Peter W. Fortescue
- 3.2 Trajectory Dynamics 51
- 3.3 General Attitude Dynamics 58
- 3.4 Attitude Motion of Specific Types of Spacecraft 63
- 3.5 Oscillatory Modes 71
- Appendix Inertia 73
- 4 Celestial Mechanics / John P. W. Stark, Graham G. Swinerd, Peter W. Fortescue
- 4.2 The Two-body Problem
- Particle Dynamics 81
- 4.3 Specifying the Orbit 91
- 4.4 Orbit Perturbations 93
- 4.5 Restricted Three-body Problem 105
- 5 Mission Analysis / John P. W. Stark, Graham G. Swinerd
- 5.2 Keplerian Orbit Transfers 114
- 5.3 Mission Analysis 116
- 5.4 Polar LEO/Remote-Sensing Satellites 122
- 5.5 Satellite Constellations 127
- 5.6 Geostationary Earth Orbits (GEO) 133
- 5.7 Highly Elliptic Orbits 143
- 5.8 Interplanetary Missions 147
- 6 Propulsion Systems / J. Barrie Moss, John P. W. Stark
- 6.1 Systems Classification 169
- 6.2 Chemical Rockets 172
- 6.3 Secondary Propulsion 193
- 6.4 Electric Propulsion 198
- 7 Launch Vehicles / J. Barrie Moss, Graham E. Dorrington
- 7.2 Basic Launch Vehicle Performance and Operation 211
- 7.3 Spacecraft Launch Phases and Mission Planning 222
- 7.4 The Ariane Launch Vehicle 226
- 7.5 The Shuttle Space Transportation System (STS) 230
- 7.6 Small Launchers 233
- 7.7 Re-Entry into Earth's Atmosphere 233
- 7.8 Specific Launch Costs and Reliability 237
- 8 Spacecraft Structures / John M. Houghton
- 8.2 Design Requirements 241
- 8.3 Design Process 257
- 8.4 Material Selection 259
- 8.5 Analysis 267
- 8.6 Design Verification 270
- 8.7 Impact Protection 272
- 8.8 Configuration Examples 274
- 8.9 The Future of Space Structures 284
- 9 Attitude Control / Peter W. Fortescue, Graham G. Swinerd
- 9.2 ACS Overview 288
- 9.3 The Spacecraft Attitude Response 292
- 9.4 Torques and Torquers 299
- 9.5 Attitude Measurement 307
- 9.6 ACS Computation 319
- 10 Electrical Power Systems / John P. W. Stark
- 10.2 Power System Elements 326
- 10.3 Primary Power Systems 328
- 10.4 Secondary Power Systems: Batteries 343
- 10.5 Power Management, Distribution and Control 346
- 10.6 Power Budget 349
- 11 Thermal Control of Spacecraft / Chris J. Savage
- 11.2 The Thermal Environment 356
- 11.3 Thermal Balance 361
- 11.4 Thermal Analysis 364
- 11.5 Thermal Design 371
- 11.6 Thermal Technology 375
- 11.7 Thermal Design Verification 385
- 11.8 Example of Satellite Thermal Design
- XMM/Newton 387
- 12 Tele-Communications / Howard Smith, Ray E. Sheriff
- 12.2 Techniques of Radio Communications 402
- 12.3 The Communications Payload 426
- 13 Telemetry, Command, Data Handling and Processing / Nigel P. Fillery, David Stanton
- 13.2 System Architecture 450
- 13.3 Telemetry Data Formatting 452
- 13.4 Telecommand 460
- 13.5 Communication Techniques and Protocols 465
- 13.6 On-Board Data Handling (OBDH) and Processing 468
- 13.7 Technology 474
- 13.8 Tools and Controlling Documents 476
- 14 Ground Stations / Richard Holdaway
- 14.2 Hardware 477
- 14.3 Software 486
- 14.4 People 494
- 14.5 Operations 494
- 14.6 Cost-Effective and Autonomous Ground Systems 495
- 14.7 Looking to the Future 499
- 15 Spacecraft Mechanisms / H. Mervyn Briscoe, Guglielmo S. Aglietti
- 15.2 One-Shot Devices 502
- 15.3 Continuously and Intermittently Operating Devices 511
- 15.4 Components 520
- 15.5 Materials 525
- 15.6 Tribology 526
- 15.7 Testing and Verification 527
- 16 Spacecraft Electromagnetic Compatibility Engineering / Ken M. Redford
- 16.2 Examples of EMC Problems 532
- 16.3 EMC Specifications 532
- 16.4 Electromagnetic Compatibility
- Terms and Definitions 533
- 16.5 EMC Fundamentals 534
- 16.6 The Systems Approach to EMC 535
- 16.7 EMC Categories 535
- 16.8 Electrostatic Discharge 539
- 16.9 Spacecraft Grounding Schemes 540
- 16.10 Major Causes of Spacecraft EMC Problems 545
- 16.11 Analysis Methods for Spacecraft EMC Engineering 546
- 17 Product Assurance / Thomas A. Meaker
- 17.2 Failures 554
- 17.3 Reliability 558
- 17.4 The Use of Qualified Parts 567
- 17.5 Materials and Processes 568
- 17.6 Safety 569
- 17.7 Configuration Control 574
- 17.8 Build and Verification 574
- Appendix 1 The Arrhenius Equation 575
- Appendix 2 Particle Radiation Data 576
- Appendix 3 De-rating 578
- 18 Small-Satellite Engineering and Applications / Martin N. Sweeting, Craig I. Underwood
- 18.2 Small-satellite Design Philosophy 585
- 18.3 Small-satellite System Design 586
- 18.4 COTS Components in the Space Environment 589
- 18.5 Microsatellite Platforms 592
- 18.6 Minisatellite Platforms 595
- 18.7 Nanosatellite Platforms 597
- 18.8 Affordable Launches for Small Satellites 599
- 18.9 In-orbit Operations 603
- 18.10 Small-satellite Applications 604
- 18.11 Picosatellites and Recent Advances in Miniaturization 610
- 19 Spacecraft System Engineering / Adrian R. L. Tatnall, John B. Farrow, C. Richard Francis
- 19.2 System Engineering 614.
- Notes:
- Includes bibliographical references and index.
- Local Notes:
- Acquired for the Penn Libraries with assistance from the Hazel M. Hussong Fund.
- ISBN:
- 0470851023
- 0471619515
- OCLC:
- 50479241
- Online:
- Publisher description
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