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Advanced Launcher Options under Constraints of Synergy, Commonality and Affordability

Sippel, Martin and Dumont, Etienne and Clark, Vanessa and Koch, Aaron and David, Emmanuelle and Garbers, Nicole and Manfletti, C. and Höck, Birte and Geiss, Gunter (2014) Advanced Launcher Options under Constraints of Synergy, Commonality and Affordability. IAC 2014, 29.09.2014-03.10.2014, Toronto, Kanada.

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Abstract

This paper addresses technical options to increase synergies between European launchers of different size. This approach should help to further improve cost competiveness though keeping the capability of serving a broad range of missions. Various combinations of stage, engine, and motor hardware exist which can be evolved or modernized to form a small to medium-size launcher. The potential future launcher options usually are an arrangement of solid and cryogenic propellant stages but with different selection for the main stages and usually a cryogenic liquid propellant upper stage with VINCI engine. DLR’s launcher analysis is focusing its research on a few promising development lines. The paper provides an overview on recent results of these activities and presents the promises and constraints of all investigated launcher configurations. Their growth potential is assessed and relative NRC and RC are presented.

Item URL in elib:https://elib.dlr.de/91272/
Document Type:Conference or Workshop Item (Speech)
Title:Advanced Launcher Options under Constraints of Synergy, Commonality and Affordability
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Sippel, Martinmartin.sippel (at) dlr.dehttps://orcid.org/0000-0001-7356-7575
Dumont, EtienneEtienne.Dumont (at) dlr.dehttps://orcid.org/0000-0003-4618-0572
Clark, VanessaVanessa.Clark (at) dlr.deUNSPECIFIED
Koch, Aaronaaron.koch (at) dlr.deUNSPECIFIED
David, Emmanuelleemmanuelle.david (at) dlr.deUNSPECIFIED
Garbers, Nicolenicole.garbers (at) dlr.deUNSPECIFIED
Manfletti, C.Chiara.Manfletti (at) dlr.deUNSPECIFIED
Höck, BirteUNSPECIFIEDUNSPECIFIED
Geiss, GunterUNSPECIFIEDUNSPECIFIED
Date:2014
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Advanced Launcher, croygenic liquid propellant upper stage, VINCI engine
Event Title:IAC 2014
Event Location:Toronto, Kanada
Event Type:international Conference
Event Dates:29.09.2014-03.10.2014
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Systemanalyse Raumtransport
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Behnke, Manuela
Deposited On:28 Oct 2014 12:29
Last Modified:31 Jul 2019 19:48

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