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Preliminary Analyses of Winged Reusable First Stages in Two- and Three-Stage to Orbit Configurations (RLVC4)

Sippel, Martin and Bussler, Leonid and Messe, Christian and Stappert, Sven and Schuster, Stephan (2020) Preliminary Analyses of Winged Reusable First Stages in Two- and Three-Stage to Orbit Configurations (RLVC4). Project Report. SART TN-015/2019. 106 S.

Full text not available from this repository.

Abstract

Semi RLV configurations are investigated with reusability of 1st or booster stages arranged in parallel with an expendable upper compartment. The non-symmetrical architecture consists of a winged RLV-stage and attached ELV-part comprising either one or two stages. The rocket propulsion is mostly cryogenic LOX-LH2 with the option of a storable propellant upper stage. The report summarizes the results of the preliminary technical design process. The overall shape and aerodynamic configuration, the propulsion and feed system, the architecture and structural lay-out of the stages are described and some indicators on the configuration’s launch cost efficiency are provided.

Item URL in elib:https://elib.dlr.de/144128/
Document Type:Monograph (Project Report)
Additional Information:Das PDF ist auf Anfrage bei RY-SRT erhältlich!
Title:Preliminary Analyses of Winged Reusable First Stages in Two- and Three-Stage to Orbit Configurations (RLVC4)
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Sippel, MartinUNSPECIFIEDhttps://orcid.org/0000-0001-7356-7575UNSPECIFIED
Bussler, LeonidUNSPECIFIEDhttps://orcid.org/0000-0002-0657-4086UNSPECIFIED
Messe, ChristianDLRUNSPECIFIEDUNSPECIFIED
Stappert, SvenUNSPECIFIEDhttps://orcid.org/0000-0002-8425-2779UNSPECIFIED
Schuster, StephanDLRUNSPECIFIEDUNSPECIFIED
Date:January 2020
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:106
Status:Published
Keywords:RLV, TSTO, trajectory, LOX-LH2-propulsion, SpaceLiner, LFBB, in-air-capturing
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 - Systems Analysis Space Transport (SART)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Vormschlag, Nele Marei
Deposited On:30 Sep 2021 11:47
Last Modified:30 Sep 2021 11:47

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