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Propulsion Systems Definition for a Liquid Fly-back Booster

Sippel, Martin and Herbertz, Armin (2007) Propulsion Systems Definition for a Liquid Fly-back Booster. 2ND EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS), 2007-07-01 - 2007-07-06, Brussels, Belgium.

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Abstract

This paper describes the final design status of a partially reusable space transportation system which has been under study for more than five years within the German future launcher technology research program ASTRA. It consists of dual booster stages, which are attached to an advanced expendable core. The design of the reference liquid fly-back boosters (LFBB) is based on LOX/LH2 propellant and a future advanced gas-generator cycle rocket motor. In focus are the four different propulsion systems and the main propellant feed and pressurization system.

Item URL in elib:https://elib.dlr.de/68076/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Propulsion Systems Definition for a Liquid Fly-back Booster
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Sippel, MartinSpace Launcher Systems Analysis (SART), DLR, 51170 Cologne, GermanyUNSPECIFIEDUNSPECIFIED
Herbertz, ArminSpace Launcher Systems Analysis (SART), DLR, 51170 Cologne, GermanyUNSPECIFIEDUNSPECIFIED
Date:2007
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Propulsion Systems, Liquid Fly-back Booster, ASTRA, LFBB, LOX/LH2 propellant motor
Event Title:2ND EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS)
Event Location:Brussels, Belgium
Event Type:international Conference
Event Start Date:1 July 2007
Event End Date:6 July 2007
Organizer:eucass
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Antriebsystemtechnik - Antriebskonzepte (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Transport and Propulsion System
Deposited By: Zierenberg, Silke
Deposited On:10 Jan 2011 11:33
Last Modified:24 Apr 2024 19:33

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