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Atllas: M6 propulsion data set, CAD model, mass estimation and trajectory analysis

Lang, A. and Sippel, M. and Klevanski, J. and Atanassov, U. (2010) Atllas: M6 propulsion data set, CAD model, mass estimation and trajectory analysis. Project Report. (Unpublished)

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Abstract

M6 is as generic supersonic passenger airplane with a cruise velocity of Mach 6. This configuration is based on the US concept HYCAT 1a. To reach the required velocity, special propulsion concepts and high capacity fuel tanks are needed. Due to aerodynamic constraints high-speed aircrafts have unconventional shapes. Hence the integration of all structure components especially the tank accommodation into the fuselage is challenging. The latest MDO design configuration (10/2008) from the Institute of Aerodynamics and Flow Technology (DLR Braunschweig) is taken as base for this work. Results of following mass estimation are e.g. gross lift off weight and CoG, which are determined by the components’ accommodation. These data are needed as input for the trajectory analysis. Finally the configuration is assessed with regard to the trajectory analysis.

Item URL in elib:https://elib.dlr.de/64889/
Document Type:Monograph (Project Report)
Title:Atllas: M6 propulsion data set, CAD model, mass estimation and trajectory analysis
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lang, A.anna.lang (at) dlr.deUNSPECIFIED
Sippel, M.martin.sippel (at) dlr.deUNSPECIFIED
Klevanski, J.josef.klevanski (at) dlr.deUNSPECIFIED
Atanassov, U.uta.atanassov (at) dlr.deUNSPECIFIED
Date:April 2010
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:M6, supersonic, airplane, Mach 6, Ma 6, HYCAT 1, HYCAT 1a, propulsion concepts, high capacity fuel tank, high-speed, aircraft, unconventional shapes, CAD, semi-detailed, mass estimtation, trajectory analysis
Institution:Institute of Space Systems
Department:Launcher Systemanalysis
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), W - Raumfahrzeugsysteme - Konzepte und Entwurf (old), W - EU Projekte Raumtransport (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Lang, Anna
Deposited On:23 Aug 2010 14:53
Last Modified:27 Sep 2016 12:10

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