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Potential Micro Launcher VLM

Dumont, Etienne and Sippel, Martin and David, Emmanuelle and Olga, Trivailo (2012) Potential Micro Launcher VLM. DLR-Interner Bericht. SART TN022/2011, 60 S. (Unpublished)

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This report sums up the orbital performance assessment of the VLM-1 launch vehicle, under study at IAE (the Brazilian Institute of Aeronautics and Space). This launcher, which is proposed to also launch SHEFEX III, is based on three solid propellant motors. The two first stages are based on a S50 stage which still has to be developed and the third stage is the S44 already in operation. It also includes an overview of existing launchers with a payload capacity of less than 1200 kg in LEO and a parametric development cost estimation of VLM-1.

Item URL in elib:https://elib.dlr.de/77328/
Document Type:Monograph (DLR-Interner Bericht)
Title:Potential Micro Launcher VLM
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Dumont, EtienneEtienne.Dumont (at) dlr.dehttps://orcid.org/0000-0003-4618-0572
Sippel, Martinmartin.sippel (at) dlr.deUNSPECIFIED
David, Emmanuelleemmanuelle.david (at) dlr.deUNSPECIFIED
Olga, Trivailoolga.trivailo (at) dlr.deUNSPECIFIED
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:60
Keywords:VLM S50 S44 Shefex Micro-launcher Cost estimation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Systemanalyse Raumtransport
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Dumont, Etienne
Deposited On:19 Nov 2012 10:38
Last Modified:27 Oct 2016 11:08

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