Manski, D. and Martin, J. A. (1990) Optimization of Propulsion Cycles for Advanced Shuttles. In: Part 2: Performance Model Methodology. 26th AIAA Propulsion Conference, 16-18 July 1990, Orlando, USA.
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Two years ago NASA and DLR computer codes were combined in order to analyse and optimize advanced rocket launcher systems. During the past year further effort has been made on this combined code concerniconcerning influences induced by the propulsive parameter such as chamber pressure, kind of cycle for the rocket motor and therefore by the required preburner pressure, mixed cycle, tripropellant cycle, nozzle extension, two-position nozzle effects etc. The emphasis of this work is to describe the performance part of the propulsion model and to apply the revised code on the optimization of single stage advanced shuttles.
|Document Type:||Conference or Workshop Item (Speech)|
|Additional Information:||LIDO-Berichtsjahr=1990, pages=15,|
|Title:||Optimization of Propulsion Cycles for Advanced Shuttles.|
|Journal or Publication Title:||Part 2: Performance Model Methodology|
|Keywords:||Rocket Cycle, Advanced Shuttle, System Analysis, Propulsion, Rocket, Launcher, Performance Model|
|Event Title:||26th AIAA Propulsion Conference, 16-18 July 1990, Orlando, USA|
|HGF - Research field:||UNSPECIFIED|
|HGF - Program:||other|
|HGF - Program Themes:||other|
|DLR - Research area:||UNSPECIFIED|
|DLR - Program:||no assignment|
|DLR - Research theme (Project):||UNSPECIFIED|
|Institutes and Institutions:||Institute of Space Propulsion > Institut für Chemische Antriebe und Verfahrenstechnik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||02 Apr 2006|
|Last Modified:||27 Apr 2009 05:31|
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