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RESOLVE: Reference Mission Scenarios for Re-usable Launcher Concepts

Wilken, Jascha and Dietlein, Ingrid Monika and Sippel, Martin and Blanco Arnao, Gonzalo and Bonetti, Davide and Pontijas Fuentes, Irene and Recupero, Cristina and Cano Torres, Álvaro (2020) RESOLVE: Reference Mission Scenarios for Re-usable Launcher Concepts. Project Report. SART TN-003/2020. 42 S.

Full text not available from this repository.

Abstract

Re-usability concept for Launch Vehicles is under investigation at different companies around the different Space Agencies since a re-usable Space Transportation Vehicle is the solution to provide interesting cost savings to achieve low-cost and reliable access to space. The term re-usable space transportation refers to several levels of reuse ranging from the entire vehicle to only parts of it. Reusability of first stages has become a standard in launch vehicle technology considering the increasing success of the key players especially from USA (Space-X with the returning of the first stage with a high-level accuracy back to Earth) but also recently from China. Europe should not obviate the challenge and identify new solutions to adequate European launchers to these new needs. For each of the technologies available (propulsion including air/breathing, aerothermodynamics and structures), this activity will identify and prototype the key equipment and components which would enable a step forward in re-usability. The intention of this project is to limit the study to re-usable first stage that will land horizontally. Different technologies will be investigated and compared in terms of subsystem impact and specifically in terms of economic impact with respect to expendable missions considering the additional costs associated to the development, manufacturing and operations.

Item URL in elib:https://elib.dlr.de/144131/
Document Type:Monograph (Project Report)
Additional Information:Das PDF ist auf Anfrage bei RY-SRT erhältlich!
Title:RESOLVE: Reference Mission Scenarios for Re-usable Launcher Concepts
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Wilken, JaschaUNSPECIFIEDhttps://orcid.org/0000-0001-5748-1261UNSPECIFIED
Dietlein, Ingrid MonikaUNSPECIFIEDhttps://orcid.org/0000-0003-4861-6317UNSPECIFIED
Sippel, MartinUNSPECIFIEDhttps://orcid.org/0000-0001-7356-7575UNSPECIFIED
Blanco Arnao, GonzaloDeimosUNSPECIFIEDUNSPECIFIED
Bonetti, DavideDeimos Space S.L.U.UNSPECIFIEDUNSPECIFIED
Pontijas Fuentes, IreneDeimosUNSPECIFIEDUNSPECIFIED
Recupero, CristinaDeimosUNSPECIFIEDUNSPECIFIED
Cano Torres, ÁlvaroDeimosUNSPECIFIEDUNSPECIFIED
Date:20 February 2020
Refereed publication:No
Open Access:No
Number of Pages:42
Status:Published
Keywords:Space Transportation Systems, Re-usable Launch Vehicle, RLV, ENTRAIN Study, Ariane Next, FESTIP
Department:RY-SRT
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - System Analysis Space Transport (SART) [RP]
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Vormschlag, Nele Marei
Deposited On:30 Sep 2021 11:56
Last Modified:30 Sep 2021 11:56

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