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Optimization of Propulsion Cycles for Advanced Shuttles.

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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Abstract

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.
Authors:
AuthorsInstitution or Email of Authors
Manski, D.UNSPECIFIED
Martin, J. A.UNSPECIFIED
Date:1990
Journal or Publication Title:Part 2: Performance Model Methodology
Status:Published
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
Location: Lampoldshausen
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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