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Atmospheric Re-Entry Vehicle Mechanics de Patrick Gallais

Atmospheric Re-Entry Vehicle Mechanics

Autor Patrick Gallais
en Limba Engleză Hardback – 18 oct 2007
Based on a long engineering experience, this book offers a comprehensive and state-of-the-art analysis of aerodynamic and flight mechanic entry topics. This updated edition had new chapters on Re-entry on Mars mission, flight quality, rarefied aerodynamics and re-entry accuracy. In addition, it provides a large set of application exercises and solutions.
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Specificații

ISBN-13: 9783540736462
ISBN-10: 3540736468
Pagini: 161
Ilustrații: XXII, 354 p.
Dimensiuni: 156 x 235 x 28 mm
Greutate: 0.68 kg
Ediția:2007
Editura: Springer Berlin, Heidelberg
Colecția Springer
Locul publicării:Berlin, Heidelberg, Germany

Public țintă

Research

Descriere

Ballistic reentry vehicles, capsules and planetary probes are the fastest human designed objects to fly through planet’s atmospheres. With velocities over Mach 20, RV’s have to dissipate a huge kinetic energy, and environment may exceed 100 g’s at center of mass, 100 bars stagnation pressure and 100 MW/m² on nosetip. Design of thermal protection system is a formidable material engineering problem. Vehicle conception covers large discipline realms, among which Aerodynamics and Flight Mechanics are essential as they only can provide necessary aeroshell shape, mass and inertia properties and tolerances to achieve adequate environment and trajectory performance. Capsules and probes have different missions and entry conditions but approaches and methods are identical. Based on a long engineering experience, this book offers a comprehensive and state of the art analysis of aerodynamic and flight mechanic entry topics. In addition, it provides a large set of application exercises and solutions. It is addressed to university and engineering school students, as well as engineers in aerospace companies and government agencies, or simply curious readers.

Cuprins

Classical Mechanics.- Topography and Gravitation.- Models of Atmosphere.- Aerodynamics.- Inertial Models.- Changing of Reference Frame.- Exoatmospheric Phase.- Six Degree-of-Freedom Reentry.- Zero Angle of Attack Reentry.- Decay of Initial Incidence.- End of the Convergence of the Incidence.- Roll-lock-in Phenomenon.- Instabilities.- Reentry Errors.

Textul de pe ultima copertă

Ballistic reentry vehicles, capsules and planetary probes are the fastest human designed objects to fly through planet’s atmospheres. With velocities over Mach 20, RV’s have to dissipate a huge kinetic energy, and environment may exceed 100 g’s at center of mass, 100 bars stagnation pressure and 100 MW/m² on nosetip. Design of thermal protection system is a formidable material engineering problem. Vehicle conception covers large discipline realms, among which Aerodynamics and Flight Mechanics are essential as they only can provide necessary aeroshell shape, mass and inertia properties and tolerances to achieve adequate environment and trajectory performance. Capsules and probes have different missions and entry conditions but approaches and methods are identical. Based on a long engineering experience, this book offers a comprehensive and state of the art analysis of aerodynamic and flight mechanic entry topics. In addition, it provides a large set of application exercises and solutions. It is addressed to university and engineering school students, as well as engineers in aerospace companies and government agencies, or simply curious readers.

Caracteristici

Comprehensive book for practitioners as students in aeronautics, written after 33years experienced and proven in first, non commercial and French edition.
New edition with new chapters on Re-entry on Mars mission, flight quality, rarefied aerodynamics and re-entry accuracy
Exercises at solutions at the end of the book