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Launcher Pre-Design: VENUS II P100 + Z40 / Z35 / Z30 + Aestus II Upper Stage

Dumont, Etienne and van Foreest, Arnold and Sippel, Martin (2010) Launcher Pre-Design: VENUS II P100 + Z40 / Z35 / Z30 + Aestus II Upper Stage. Project Report. SART TN-001/2010. DLR Institut für Raumfahrtsysteme. 83 S. (Unpublished)

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This technical report gives a brief overview of the preliminary design of new, liquid fuelled upper stages for a launcher based on VEGA. The report describes the different concepts based on P100, Z30/Z35/Z40 and Aestus II in the framework of the VENUS II DLR-EADS contract and their current component mass data (status December 2009). Optimal propellant masses for the upper stages and sensitivity are determined. Performance and trajectories are calculated for each studied configuration. In addition the results of the CEF study are presented and include mass breakdowns, maximum payload masses and trajectory analyses.

Item URL in elib:https://elib.dlr.de/64761/
Document Type:Monograph (Project Report)
Title:Launcher Pre-Design: VENUS II P100 + Z40 / Z35 / Z30 + Aestus II Upper Stage
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Dumont, EtienneUNSPECIFIEDhttps://orcid.org/0000-0003-4618-0572UNSPECIFIED
Date:15 June 2010
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:83
Keywords:VENUS II, VEGA, evolution, liquid upper stage, propulsion, Aestus II, P100, Z40, Z35, Z30
Institution:DLR Institut für Raumfahrtsysteme
Department:Systemanalyse Raumtransport
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Raumfahrzeugsysteme - Systemanalyse Raumtransport (old), W - Zukünftige Raumtransporter - Entwurf und Simulationsmethoden für Raumtransporter (old), W - Raumfahrzeugsysteme - Konzepte und Entwurf (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Dumont, Etienne
Deposited On:23 Jul 2010 10:44
Last Modified:27 Oct 2016 11:03

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