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A Trendsetting Micro-Launcher for Europe

Gamgami, Farid (2009) A Trendsetting Micro-Launcher for Europe. 3rd EUCASS 2009, 6-9 Juli 2009, Versailles Frankreich. (Unpublished)

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Abstract

In this paper we analyse a potential, future European launcher for micro payloads (200kg in LEO). This study comprises ascent trajectory calculation, aerodynamics and mass estimation. The most remarkable feature is the reusable first stage (RFS). Therefore, beside the ascent analyses, reentry calculations have also been performed. To bring the first stage back to an airbase we suggest in-air capturing. In addition to the technical performance analyses we discuss the potential this kind of launcher has for European space transportation.

Item URL in elib:https://elib.dlr.de/61282/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:A Trendsetting Micro-Launcher for Europe
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gamgami, FaridFarid.Gamgami (at) dlr.deUNSPECIFIED
Date:9 July 2009
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:reusable first stage, micro launcher, in air capturing, winged re-entry
Event Title:3rd EUCASS 2009
Event Location:Versailles Frankreich
Event Type:international Conference
Event Dates:6-9 Juli 2009
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 - Raumfahrzeugsysteme - Systemanalyse Raumtransport (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Gamgami, Farid
Deposited On:02 Dec 2009 11:43
Last Modified:31 Jul 2019 19:26

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