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Preliminary Definition of an Aerodynamic Configuration for a Reusable Booster Stage within Tight Geometric Constraints

Sippel, M. and Klevanski, J. (2004) Preliminary Definition of an Aerodynamic Configuration for a Reusable Booster Stage within Tight Geometric Constraints. In: 5th European Symposium on Aerothermodynamics for Space, pp. 1-6. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln, 08.-11. Nov. 2004.

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Item URL in elib:https://elib.dlr.de/1722/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2004,
Title:Preliminary Definition of an Aerodynamic Configuration for a Reusable Booster Stage within Tight Geometric Constraints
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Sippel, M.UNSPECIFIEDUNSPECIFIED
Klevanski, J.UNSPECIFIEDUNSPECIFIED
Date:2004
Journal or Publication Title:5th European Symposium on Aerothermodynamics for Space
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-6
Editors:
EditorsEmail
DLR, UNSPECIFIED
Status:Published
Event Title:5th European Symposium on Aerothermodynamics for Space Vehicles, Köln, 08.-11. Nov. 2004
Organizer:DLR
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):E - no assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Lohmiller, Monika
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 14:11

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