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Feasibility of High Thrust Bleed Cycle Engines for Reusable Booster Applications

Sippel, M. and Herbertz, A. and Haeseler, D. and Götz, A. (2002) Feasibility of High Thrust Bleed Cycle Engines for Reusable Booster Applications. In: 4th International Conference on Launcher Technology "Space Launcher Liquid Propulsion". 4th International Conference on Launcher Technology "Space Launcher Liquid Propulsion", Liege, 3 - 6 December 2002.

Full text not available from this repository.

Abstract

Based on results of an earlier cycle analysis, an improved engine variant of a high thrust, cryogenic bleed cycle engine is analyzed. Its performance is calculated, and a preliminary engine sizing and mass analysis is carried out. Improvement options as well as growth potential of the cycle is investigated with special regard to the critical heat-transfer in the thrust chamber region. Finally, an ascent trajectory optimization and a discussion of the complete vehicle are performed to evaluate the engines as part of a future semi reusable launch system.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2003,
Title:Feasibility of High Thrust Bleed Cycle Engines for Reusable Booster Applications
Authors:
AuthorsInstitution or Email of Authors
Sippel, M.UNSPECIFIED
Herbertz, A.UNSPECIFIED
Haeseler, D.UNSPECIFIED
Götz, A.UNSPECIFIED
Date:2002
Journal or Publication Title:4th International Conference on Launcher Technology "Space Launcher Liquid Propulsion"
Editors:
EditorsEmail
CNES, UNSPECIFIED
Status:Published
Event Title:4th International Conference on Launcher Technology "Space Launcher Liquid Propulsion", Liege, 3 - 6 December 2002
Organizer:Centre National D'Etudes Spatiales (CNES)
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 assignement
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Monika Lohmiller
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 14:01

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