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Aerodynamic Design of an Ariane 5 Liquid Fly-Back Booster

Eggers, T. (2002) Aerodynamic Design of an Ariane 5 Liquid Fly-Back Booster.

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Within the German future space launcher technology research program ASTRA two reusable first stage designs are under investigation. The one dedicated for near term application with an existing expendable core stage is called a winged liquid fly-back booster (LFBB). The main goal of the present study is the refinement of an existing LFBB design. The regarded partially reusable space transportation system consists of two booster stages, which are attached to the expendable Ariane 5 core stage at an upgraded future technology level. The area of interest discussed here is the descent after the staging procedure which dominates the aerodynamic design of the LFBB. The aerodynamic parameter studies pointed out that an LFBB may not be trimmed or stabilised without the introduction of canards as control surface. By introduction of canards a more robust configuration is obtained.

Item URL in elib:https://elib.dlr.de/12519/
Document Type:Article
Additional Information: LIDO-Berichtsjahr=2003,
Title:Aerodynamic Design of an Ariane 5 Liquid Fly-Back Booster
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:Yes
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
Keywords:aerodynamic design, subsonic, transonic, super- and hypersonic, aerodynamics, flight mechanics
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 - Grundlagen Raumtransport - Anlagen und Messtechnik (old)
Location: Köln-Porz , Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology
Deposited By: Grant, Claudia
Deposited On:12 Jan 2006
Last Modified:22 Jan 2018 16:49

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