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Experimental investigation on the draining behavior in scaled models of the new A5ME upper stage propellant compartments with respect to different flight conditions

Fischer, A. and Gerstmann, Jens and Haake, D. and Goossens, T. (2014) Experimental investigation on the draining behavior in scaled models of the new A5ME upper stage propellant compartments with respect to different flight conditions. DLRK 2014, 16.-18.09.2014, Augsburg. (Unpublished)

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Abstract

The maximum possible mass, launched to orbit by a rocket, depends on the launcher performance and the desired target orbit. To provide as much capacity to the payload as possible, the total mass of the launchers upper stage has to be minimized. Intelligent propellant management can contribute significantly to increase the performance of the launcher. To optimize the flight missions the tank outlet design is required, to achieve that a maximum of the propellant is available for the mission and a minimum of propellant loading remains as unused residual.

Item URL in elib:https://elib.dlr.de/103002/
Document Type:Conference or Workshop Item (Speech)
Title:Experimental investigation on the draining behavior in scaled models of the new A5ME upper stage propellant compartments with respect to different flight conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Fischer, A.UNSPECIFIEDUNSPECIFIED
Gerstmann, JensUNSPECIFIEDUNSPECIFIED
Haake, D.UNSPECIFIEDUNSPECIFIED
Goossens, T.UNSPECIFIEDUNSPECIFIED
Date:2014
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:A5ME, upper stage propellant
Event Title:DLRK 2014
Event Location:Augsburg
Event Type:national Conference
Event Dates:16.-18.09.2014
Organizer:DGLR
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:other
DLR - Research area:Raumfahrt
DLR - Program:R - no assignment
DLR - Research theme (Project):R - no assignment
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Transport and Propulsion System
Deposited By: Behnke, Manuela
Deposited On:24 Feb 2016 09:40
Last Modified:31 Jul 2019 20:00

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