DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Family of Launchers Approach vs. “Big-Size-Fits-All”

Sippel, Martin and Stappert, Sven and Callsen, Steffen and Bergmann, Kevin and Dietlein, Ingrid Monika and Bussler, Leonid (2022) Family of Launchers Approach vs. “Big-Size-Fits-All”. International Astronautical Congress (IAC 2022), 2022-09-18 - 2022-09-22, Paris, France.

[img] PDF


One option for future space transportation concepts could be a family of launchers supporting a wide range of payload performance. The idea bases upon using “building blocks” of common stages or main propulsion rocket engines and applying them in a modular way. A somehow contrarious option is a single TSTO launch vehicle serving all kinds of missions, even those which have payload mass requirements much below the design capacity. The technical investigations described in this paper evaluate the two antipodal design approaches of either establishing a launcher family consisting of modular building blocks or choosing a full-size launcher which serves all missions with minimal adaptations of the upper- and kick-stage selection. The paper summarizes major results of the preliminary technical design process. The overall shape and aerodynamic configuration, the propulsion and feed system, the architecture of the stages are described and different technical solutions are compared. Payload performance is optimized for the different concepts in the GTO-mission, manned flight to ISS and to SSO. The winged configurations’ controllability in hypersonic reentry and subsequent subsonic flight is assessed. The study is completed by a relative comparison of to be expected RC/NRC of the different launcher concepts.

Item URL in elib:https://elib.dlr.de/195201/
Document Type:Conference or Workshop Item (Speech)
Title:Family of Launchers Approach vs. “Big-Size-Fits-All”
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Sippel, MartinUNSPECIFIEDhttps://orcid.org/0000-0001-7356-7575UNSPECIFIED
Stappert, SvenDLRhttps://orcid.org/0000-0002-8425-2779UNSPECIFIED
Callsen, SteffenUNSPECIFIEDhttps://orcid.org/0000-0002-5481-5403160064750
Bergmann, KevinUNSPECIFIEDhttps://orcid.org/0000-0003-1387-6223UNSPECIFIED
Dietlein, Ingrid MonikaUNSPECIFIEDhttps://orcid.org/0000-0003-4861-6317UNSPECIFIED
Bussler, LeonidUNSPECIFIEDhttps://orcid.org/0000-0002-0657-4086UNSPECIFIED
Date:18 September 2022
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In ISI Web of Science:No
Keywords:RLV, LOX-LH2-propulsion, LOX-LCH4-propulsion, VTHL, VTVL, in-air-capturing
Event Title:International Astronautical Congress (IAC 2022)
Event Location:Paris, France
Event Type:international Conference
Event Start Date:18 September 2022
Event End Date:22 September 2022
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 - Reusable Space Systems and Propulsion Technology, 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:25 May 2023 09:29
Last Modified:22 May 2024 09:16

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.