Fundamentals of Space Systems
Series: Johns Hopkins University Applied Physics Laboratories Series in Science and Engineering;
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Product details:
- Edition number 2
- Publisher OUP USA
- Date of Publication 17 March 2005
- ISBN 9780195162059
- Binding Hardback
- No. of pages848 pages
- Size 155x244x44 mm
- Weight 1293 g
- Language English
- Illustrations 7 halftones, 348 line illus. 0
Categories
Short description:
Fundamentals of Space Systems is suitable for use in undergraduate or graduate courses in space systems engineering or space system design and as a primer and reference book for space professionals. The authors present the material in a manner that benefits from their experience as practicing engineers with extensive experience in developing sophisticated experimental and operational spacecraft systems.
MoreLong description:
Fundamentals of Space Systems was developed to satisfy two objectives: the first is to provide a text suitable for use in an advanced undergraduate or beginning graduate course in both space systems engineering and space system design. The second is to be a primer and reference book for space professionals wishing to broaden their capabilities to develop, manage the development, or operate space systems. The authors of the individual chapters are practicing engineers that have had extensive experience in developing sophisticated experimental and operational spacecraft systems in addition to having experience teaching the subject material. The text presents the fundamentals of all the subsystems of a spacecraft missions and includes illustrative examples drawn from actual experience to enhance the learning experience. It included a chapter on each of the relevant major disciplines and subsystems including space systems engineering, space environment, astrodynamics, propulsion and flight mechanics, attitude determination and control, power systems, thermal control, configuration management and structures, communications, command and telemetry, data processing, embedded flight software, survuvability and reliability, integration and test, mission operations, and the initial conceptual design of a typical small spacecraft mission.
MoreTable of Contents:
Chapter 1: Systems Engineering and Management
Chapter 2: The Space Environment
Chapter 3: Astrodynamics
Chapter 4: Spacecraft Propulsion, Launch Systems, and Launch Mechanics
Chapter 5: Spacecraft Attitude and Determination Control
Chapter 6: Space Power Systems
Chapter 7: Spacecraft Thermal Control
Chapter 8: Spacecraft Configuration and Structural Design
Chapter 9: Space Communications
Chapter 10: Spacecraft Command and Telemetry
Chapter 11: Spacecraft Computer Systems
Chapter 12: Embedded Software Systems
Chapter 13: Spacecraft Reliability
Chapter 14: Spacecraft Integration and Test
Chapter 15: Space Mission Operations
Chapter 16: Nanosatellite Conceptual Design
