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Callisto Flight Demonstrator Options winged vs. ballistic

Bussler, Leonid and Stappert, Sven and Sippel, Martin and Garbers, Nicole (2017) Callisto Flight Demonstrator Options winged vs. ballistic. Project Report. SART TN-016/2016. 90 S.

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Different flight demonstrator options including winged and non-winged configurations are investigated. The expander cycle engines RSR of Japan and the European Vinci are considered as available rocket propulsion options. All configurations are sized with preliminary design methods and are subsequently simulated for missions from Kourou.

Item URL in elib:https://elib.dlr.de/144100/
Document Type:Monograph (Project Report)
Additional Information:Das PDF ist auf Anfrage bei RY-SRT erhältlich!
Title:Callisto Flight Demonstrator Options winged vs. ballistic
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Bussler, LeonidUNSPECIFIEDhttps://orcid.org/0000-0002-0657-4086UNSPECIFIED
Stappert, SvenUNSPECIFIEDhttps://orcid.org/0000-0002-8425-2779UNSPECIFIED
Sippel, MartinUNSPECIFIEDhttps://orcid.org/0000-0001-7356-7575UNSPECIFIED
Date:July 2017
Refereed publication:No
Open Access:No
Number of Pages:90
Keywords:RLV flight demonstrators, Vinci, RSR, Larcac 04, in-air-capturing, Callisto, VTOHL, VTOL
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:29 Sep 2021 12:16
Last Modified:29 Sep 2021 12:16

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