Basic Research and Technologies for Two-Stage-to-Orbit Vehicles
Collaborative Research Centre
(Sprache: Englisch)
Focusing on basic aspects of future reusable space transportation systems and covering overall design, aerodynamics, thermodynamics, flight dynamics, propulsion, materials, and structures, this report presents some of the most recent results obtained in...
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Focusing on basic aspects of future reusable space transportation systems and covering overall design, aerodynamics, thermodynamics, flight dynamics, propulsion, materials, and structures, this report presents some of the most recent results obtained in these disciplines. The authors are members of three Collaborative Research Centers in Aachen, Munich and Stuttgart concerned with hypersonic vehicles.A major part of the research presented here deals with experimental and numerical aerodynamic topics ranging from low speed to hypersonic flow past the external configuration and through inlet and nozzle. Mathematicians and engineers jointly worked on aspects of flight mechanics like trajectory optimization, stability, control and flying qualities. Structural research and development was predominantly coupled to the needs for high temperature resistant structures for space vehicles.
Focusing on basic aspects of future reusable space transportation systems and covering overall design, aerodynamics, thermodynamics, flight dynamics, propulsion, materials, and structures, this report presents some of the most recent results obtained in these disciplines. The authors are members of three Collaborative Research Centers in Aachen, Munich and Stuttgart concerned with hypersonic vehicles.
A major part of the research presented here deals with experimental and numerical aerodynamic topics ranging from low speed to hypersonic flow past the external configuration and through inlet and nozzle. Mathematicians and engineers jointly worked on aspects of flight mechanics like trajectory optimization, stability, control and flying qualities. Structural research and development was predominantly coupled to the needs for high temperature resistant structures for space vehicles.
A major part of the research presented here deals with experimental and numerical aerodynamic topics ranging from low speed to hypersonic flow past the external configuration and through inlet and nozzle. Mathematicians and engineers jointly worked on aspects of flight mechanics like trajectory optimization, stability, control and flying qualities. Structural research and development was predominantly coupled to the needs for high temperature resistant structures for space vehicles.
Inhaltsverzeichnis zu „Basic Research and Technologies for Two-Stage-to-Orbit Vehicles “
PrefaceNetwork Organization of Collaborative Research Centers for Scientific Efficiency Enhancement
Overall Design Aspects
Aerodynamics and Thermodynamics
Propulsion
Flight Mechanics and Control
High-Temperature Materials and Hot Structures
Cooperation with Industry and Research Establishments, Participation in National and International Research Programs
Conclusions and Perspectives
Appendix
Autoren-Porträt
Prof. Dr. Gottfried Sachs wurde 1977 an die Universität der Bundeswehr München berufen. 1983 folgt er einem Ruf an die TU München. Der Ordinarius für Flugmechanik und Flugregelung ist seit 1998 Fellow des American Institute of Aeronautics and Astronautics und seit 2004 Mitglied des Vorstandes der Bayerischen Akademie der Wissenschaften.
Bibliographische Angaben
- 2005, 1. Auflage, XVII, 666 Seiten, 31 farbige Abbildungen, 381 Schwarz-Weiß-Abbildungen, Maße: 18 x 24,5 cm, Kartoniert (TB), Englisch
- Herausgegeben: Dieter Jacob, Gottfried Sachs, Siegfried Wagner
- Verlag: Wiley-VCH
- ISBN-10: 3527277358
- ISBN-13: 9783527277353
Sprache:
Englisch
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