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ATLLAS: M3 CAD- and mass-model

Lang, A. and Atanassov, U. and Sippel, M. and Koch, A. (2010) ATLLAS: M3 CAD- and mass-model. Project Report. Institute of Space Systems. (Unpublished)

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Abstract

Within the ATLLAS (Aerodynamic and Thermal Load Interactions with Lightweight Advanced Materials for High Speed Flight) a 200-seat SST concept will be designed in WP 2.3 to meet an operational requirement of Mach 3 flight over a 5500 nm range. The Mach 3 speed range allows consideration of established materials and newer materials. The Mach 3 vehicle will be designed along the principles outlined in WP2.1 and WP2.2 by GDL and system mass and payload fraction will be predicted by DLR-SART and GDL respectively. DLR-SART provides the creation and the iterative adaptation of the semi-detailed CAD-representation of the Mach 3 SST-vehicle in support of the design process. The objective of this report in support of deliverable D2.3.3 is the description of the semi-detailed CAD model for the M3 configuration. In addition to this model a mass estimation is done and a calculation and the CoG shifting is analysed.

Item URL in elib:https://elib.dlr.de/64884/
Document Type:Monograph (Project Report)
Title:ATLLAS: M3 CAD- and mass-model
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Lang, A.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Atanassov, U.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Sippel, M.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Koch, A.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:April 2010
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:Atllas, SST, supersonic, airplane, M3, SART, mass estimation, high speed flight, Mach 3, Ma 3, semi-detailed, CAD, CoG shifting
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 16:00
Last Modified:31 Jul 2019 19:28

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