Aerodynamic and Aerothermodynamic Analysis of Space Mission Vehicles

Presenting an up-to-date view on the most important space vehicle configurations, this book contains detailed analyses for several different type of space mission profiles while considering important factors such as aerodynamic loads, aerodynamic heating, vehicle stability and landing characteristic...

Πλήρης περιγραφή

Λεπτομέρειες βιβλιογραφικής εγγραφής
Κύριοι συγγραφείς: Viviani, Antonio (Συγγραφέας), Pezzella, Giuseppe (Συγγραφέας)
Συγγραφή απο Οργανισμό/Αρχή: SpringerLink (Online service)
Μορφή: Ηλεκτρονική πηγή Ηλ. βιβλίο
Γλώσσα:English
Έκδοση: Cham : Springer International Publishing : Imprint: Springer, 2015.
Σειρά:Springer Aerospace Technology,
Θέματα:
Διαθέσιμο Online:Full Text via HEAL-Link
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100 1 |a Viviani, Antonio.  |e author. 
245 1 0 |a Aerodynamic and Aerothermodynamic Analysis of Space Mission Vehicles  |h [electronic resource] /  |c by Antonio Viviani, Giuseppe Pezzella. 
264 1 |a Cham :  |b Springer International Publishing :  |b Imprint: Springer,  |c 2015. 
300 |a XXII, 898 p. 842 illus., 170 illus. in color.  |b online resource. 
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490 1 |a Springer Aerospace Technology,  |x 1869-1730 
505 0 |a Basics of Hypersonic Aerodynamics and Aerothermodynamics -- Fundamentals of Atmospheric Entry Dynamics -- Some Preliminary Considerations on Entry Vehicle Design -- Analysis of an Apollo-shaped Crew Return Vehicle -- Lifting-body Vehicles -- Winged Re-Entry Vehicles -- Analysis of Sample Return Capsules -- Launchers: Present and Future -- Appendices. 
520 |a Presenting an up-to-date view on the most important space vehicle configurations, this book contains detailed analyses for several different type of space mission profiles while considering important factors such as aerodynamic loads, aerodynamic heating, vehicle stability and landing characteristics. With that in mind, the authors provide a detailed overview on different state-of-the-art themes of hypersonic aerodynamics and aerothermodynamics, and consider different space vehicle shapes useful for different space mission objectives. These include: ·        Crew Return Vehicle (CRV) ·        Crew Exploration Vehicle (CEV) ·        Sample Return Vehicle (SRV) ·        Flying Test Bed (FTB). Throughout Aerodynamic and Aerothermodynamic Analysis of Space Mission Vehicles many examples are given, with detailed computations and results for the aerodynamics and aerothermodynamics of all such configurations. Moreover, a final chapter on future launchers is provided and an Appendix on a possible manned mission to Mars closes the book. This work can be used as a reference for modelling and design techniques, for students intending to enter aerospace industrial careers, and to support both academics and engineers working in the field of space vehicle design. 
650 0 |a Engineering. 
650 0 |a Thermodynamics. 
650 0 |a Fluid mechanics. 
650 0 |a Aerospace engineering. 
650 0 |a Astronautics. 
650 0 |a Control engineering. 
650 1 4 |a Engineering. 
650 2 4 |a Aerospace Technology and Astronautics. 
650 2 4 |a Thermodynamics. 
650 2 4 |a Control. 
650 2 4 |a Engineering Fluid Dynamics. 
700 1 |a Pezzella, Giuseppe.  |e author. 
710 2 |a SpringerLink (Online service) 
773 0 |t Springer eBooks 
776 0 8 |i Printed edition:  |z 9783319139265 
830 0 |a Springer Aerospace Technology,  |x 1869-1730 
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950 |a Engineering (Springer-11647)