Basic Research and Technologies for Two-Stage-to-Orbit Vehicles: Final Report of the Collaborative Research Centres 253, 255 and 259

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Dieter Jacob, Gottfried Sachs, Siegfried Wagner
John Wiley & Sons, Mar 6, 2006 - Technology & Engineering - 683 pages
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.

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1 Introduction
2 Network Organization of Collaborative Research Centres for Scientific Efficiency Enhancement
3 Overall Design Aspects
4 Aerodynamics and Thermodynamics
5 Propulsion
6 Flight Mechanics and Control
7 HighTemperature Materials and Hot Structures
8 Cooperation with Industry and Research Establishments Participation in National and International Research Programmes
9 Conclusions and Perspectives
10 Appendix

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About the author (2006)

Dieter Jacob holds the chair of Construction Management at the Technical University Freiberg. Aside from that he runs his own engineering and consulting office. He is author and editor of various books on estimating in construction. Clemens Muller, MSc, is a research associate at the chair of Construction Management at the Technical University Freiberg.

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