Elements of space technology for aerospace engineers
- Rudolf X. Meyer.
- San Diego : Academic Press, c1999.
- Physical description
- xi, 329 p. : ill. ; 27 cm.
- Meyer, Rudolph X.
- Includes bibliographical references and index.
- Preface. Reference Frames and Time. Reference Frames. Motion in Accelerated Reference Frames. Example: The Yo-Yo Despin Mechanism. Euler Angles and Transformations of Coordinates. Time Intervals and Epoch. Forces and Moments. Gravity. Thrust. Aerodynamic Forces and Moments. Free Molecule Flow. Solar Radiation Pressure. Atmospheric Entry. Orbits and Trajectories in an Inverse Square Field. Kepler Orbits and Trajectories. Position as a Function of Time. D'Alembert and Fourier-Bessel Series. Orbital Elements. Spacecraft Visibility Above the Horizon. Satellite Observations and the f and g Series. Special Orbits. Perturbations by Other Astronomical Bodies. Planetary Fly-By and Gravity Assist. Relativistic Effects. Chemical Rocket Propulsion. Configurations of Liquid-Propellant Chemical Rocket Motors. Configurations of Solid-Propellant Motors. Rocket Stages. Idealized Model of Chemical Rocket Motors. Ideal Thrust. Rocket Motor Operation in the Atmosphere. Two and Three-Dimensional Effects. Critique of the Ideal Model. Elements of Chemical Kinetics. Chemical Kinetics Applications to Rocket Motors Liquid Propellants. Propellant Tanks. Propellant Feed systems of Launch Vehicles. Thrust Chambers of Liquid-Propellant Motors. Pogo Instability and Prevention. Thrust Vector Control. Engine Control and Operations. Liquid-Propellant Motors and Thrusters on Spacecraft. Components of Solid-Propellant Rocket Motors. Hybrid-Propellant Rocket Motors. Orbital Maneuvers. Minimum Energy Paths. Lambert's Theorem. Maneuvers with Impulsive Thrust. Hohmann Transfers. Other Transfer Trajectories. On-Orbit Drift. Launch Windows. Injection Errors and Their Corrections. On-Orbit Phase Changes. Rendez-Vous Maneuvers. Gravity Turn. Attitude Control. Principal Axes and Moments of Inertia of Spacecraft. The Euler Equations for Time-Dependent Moments of Inertia. The Torque-Free Spinning Body. Attitude Control Sensors. Attitude Control Actuators. Spin-Stablilized Vehicles. Gravity Gradient Stabilization. Spacecraft Thermal Design. Fundamentals of Thermal Radiation. Spacecraft Surface Materials. Model of a Spacecraft as an Isothermal Sphere. Earth Thermal Radiation and Albedo. Diurnal and Annual Variations of Solar Heating. Thermal Blankets. Thermal Conduction. Lumped Parameter Model of a Spacecraft. Thermal Control Devices. Bibliography. Appendix.
- (source: Nielsen Book Data)
- Publisher's Summary
- This book is written for an introductory course in space technology. It is intended for senior or graduate level aerospace engineering students and professional engineers seeking a thorough understanding of the aerospace aspects of space systems. As such, it focuses on the primary physics and engineering fundamentals necessary to understand and design space based systems. The book does not include the basics of spacecraft electronics, because this is covered in many systems and electronics books and is typically covered in follow-up courses. It is derived from the author's thirty years of experience in the aerospace industry and several years of university teaching experience. It contains more than 130 illustrations. Advanced subjects and problems indicated by asterisks (*) allow the reader and the instructor to omit topics without losing continuity. All chapters correspond to the engineering subdivisions typically found in the aerospace industry. It includes United States and international technologies. It features an extensive appendix of important data, not easily located in other sources. The book does not include the basics of spacecraft electronics.
(source: Nielsen Book Data)
- Publication date
- Title Variation
- Elements of space technology