Synopsis
Design of a space launch vehicle is a very challenging and long running activity because of highly complex and interconnected nature of the launch vehicles. In the frame of this study, it was aimed to develop a quick and effective tool to find optimal vehicle configurations in the early design phases. First, a trajectory optimization code utilizing a general purpose optimal control solver GPOPS-II® was developed to determine the optimal trajectory in terms of position and velocity, and the control functions corresponding to that trajectory while maximizing the payload mass. Next, a staging optimization code was developed to determine the staging parameters (number of stages, mass distribution between stages, and the propellant and structural mass of each individual stage) which minimize the gross lift-off mass. Finally, these two codes were integrated for simultaneous optimization of the thrust and mass profile of the stages together with the trajectory of the launch vehicle. This newly developed tool can be utilized both for preliminary mission design of an existing launch vehicle and conceptual design of a new launch vehicle.
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Space Launcher Design with Thrust Profile and Trajectory Optimization
Edité par
LAP LAMBERT Academic Publishing Jul 2018, 2018
ISBN 10 : 6139879221
ISBN 13 : 9786139879229
Neuf
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Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Design of a space launch vehicle is a very challenging and long running activity because of highly complex and interconnected nature of the launch vehicles. In the frame of this study, it was aimed to develop a quick and effective tool to find optimal vehicle configurations in the early design phases. First, a trajectory optimization code utilizing a general purpose optimal control solver GPOPS-II® was developed to determine the optimal trajectory in terms of position and velocity, and the control functions corresponding to that trajectory while maximizing the payload mass. Next, a staging optimization code was developed to determine the staging parameters (number of stages, mass distribution between stages, and the propellant and structural mass of each individual stage) which minimize the gross lift-off mass. Finally, these two codes were integrated for simultaneous optimization of the thrust and mass profile of the stages together with the trajectory of the launch vehicle. This newly developed tool can be utilized both for preliminary mission design of an existing launch vehicle and conceptual design of a new launch vehicle. 268 pp. Englisch. N° de réf. du vendeur 9786139879229
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Space Launcher Design with Thrust Profile and Trajectory Optimization
Edité par
LAP LAMBERT Academic Publishing, 2018
ISBN 10 : 6139879221
ISBN 13 : 9786139879229
Neuf
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Vendeur : moluna, Greven, Allemagne
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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Civek-Coskun EzgiEzgi Civek-Coskun received the BS, MS and PhD degrees in mechanical engineering from the Middle East Technical University, Turkey, in 2003, 2006 and 2014 respectively. She began her professional career as a propulsio. N° de réf. du vendeur 385875547
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Space Launcher Design with Thrust Profile and Trajectory Optimization
Edité par
LAP LAMBERT Academic Publishing, 2018
ISBN 10 : 6139879221
ISBN 13 : 9786139879229
Neuf
Taschenbuch
Vendeur : preigu, Osnabrück, Allemagne
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Taschenbuch. Etat : Neu. Space Launcher Design with Thrust Profile and Trajectory Optimization | Ezgi Civek-Co¿kun | Taschenbuch | 268 S. | Englisch | 2018 | LAP LAMBERT Academic Publishing | EAN 9786139879229 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. N° de réf. du vendeur 114206660
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Space Launcher Design with Thrust Profile and Trajectory Optimization
Edité par
LAP LAMBERT Academic Publishing Jul 2018, 2018
ISBN 10 : 6139879221
ISBN 13 : 9786139879229
Neuf
Taschenbuch
Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne
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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -Design of a space launch vehicle is a very challenging and long running activity because of highly complex and interconnected nature of the launch vehicles. In the frame of this study, it was aimed to develop a quick and effective tool to find optimal vehicle configurations in the early design phases. First, a trajectory optimization code utilizing a general purpose optimal control solver GPOPS-II® was developed to determine the optimal trajectory in terms of position and velocity, and the control functions corresponding to that trajectory while maximizing the payload mass. Next, a staging optimization code was developed to determine the staging parameters (number of stages, mass distribution between stages, and the propellant and structural mass of each individual stage) which minimize the gross lift-off mass. Finally, these two codes were integrated for simultaneous optimization of the thrust and mass profile of the stages together with the trajectory of the launch vehicle. This newly developed tool can be utilized both for preliminary mission design of an existing launch vehicle and conceptual design of a new launch vehicle.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 268 pp. Englisch. N° de réf. du vendeur 9786139879229
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Space Launcher Design with Thrust Profile and Trajectory Optimization
Edité par
LAP LAMBERT Academic Publishing, 2018
ISBN 10 : 6139879221
ISBN 13 : 9786139879229
Neuf
Paperback
Vendeur : Revaluation Books, Exeter, Royaume-Uni
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Paperback. Etat : Brand New. 268 pages. 8.66x5.91x0.61 inches. In Stock. N° de réf. du vendeur zk6139879221
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Space Launcher Design with Thrust Profile and Trajectory Optimization
Edité par
LAP LAMBERT Academic Publishing, 2018
ISBN 10 : 6139879221
ISBN 13 : 9786139879229
Neuf
Taschenbuch
Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Design of a space launch vehicle is a very challenging and long running activity because of highly complex and interconnected nature of the launch vehicles. In the frame of this study, it was aimed to develop a quick and effective tool to find optimal vehicle configurations in the early design phases. First, a trajectory optimization code utilizing a general purpose optimal control solver GPOPS-II® was developed to determine the optimal trajectory in terms of position and velocity, and the control functions corresponding to that trajectory while maximizing the payload mass. Next, a staging optimization code was developed to determine the staging parameters (number of stages, mass distribution between stages, and the propellant and structural mass of each individual stage) which minimize the gross lift-off mass. Finally, these two codes were integrated for simultaneous optimization of the thrust and mass profile of the stages together with the trajectory of the launch vehicle. This newly developed tool can be utilized both for preliminary mission design of an existing launch vehicle and conceptual design of a new launch vehicle. N° de réf. du vendeur 9786139879229
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Space Launcher Design with Thrust Profile and Trajectory Optimization
Edité par
LAP LAMBERT Academic Publishing, 2018
ISBN 10 : 6139879221
ISBN 13 : 9786139879229
Neuf
paperback
Vendeur : Mispah books, Redhill, SURRE, Royaume-Uni
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paperback. Etat : New. NEW. SHIPS FROM MULTIPLE LOCATIONS. book. N° de réf. du vendeur ERICA82961398792216
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