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Computational Model of a Hybrid Propulsion System on a Robotic Lunar Lander

Escrigas, Oriol (2016) Computational Model of a Hybrid Propulsion System on a Robotic Lunar Lander. Bachelor's. DLR-Interner Bericht. DLR-IB-RA-LA-2016-257.

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Item URL in elib:https://elib.dlr.de/107042/
Document Type:Monograph (DLR-Interner Bericht, Bachelor's)
Title:Computational Model of a Hybrid Propulsion System on a Robotic Lunar Lander
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Escrigas, OriolRA-RAK LAUNSPECIFIED
Date:2016
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hybrid propulsion, rocket combustion
Institution:RWTH Aachen
Department:Institut für Strahlantriebe und Turboarbeitsmaschinen
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 - Antriebsystemtechnik - Schubkammertechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:26 Oct 2016 07:38
Last Modified:26 Oct 2016 07:38

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