Basic Research And Technologies for Two-stage-to-orbit Vehicles: Final Report of the Collaborative Research Centres 253, 255 And 259

Basic Research And Technologies for Two-stage-to-orbit Vehicles: Final Report of the Collaborative Research Centres 253, 255 And 259

by: Dieter Jacob (Author),Gottfried Sachs(Author),Siegfried Wagner(Author)&0more

Publisher: Vch Verlagsgesellschaft Mbh

Edition: 1st

Publication Date: 2005/12/2

Language: English

Print Length: 684 pages

ISBN-10: 3527277358

ISBN-13: 9783527277353

Book Description

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 conceed 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 exteal 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.

About the Author

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 conceed 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 exteal 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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