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Systems Analysis of a High Thrust, Low-Cost Rocket Engine

Kauffmann, J. and Herbertz, A. and Sippel, M. (2001) Systems Analysis of a High Thrust, Low-Cost Rocket Engine. In: Fourth International Conference on Green Propellants for Space Propulsion. 4th International Conference on Green Propellants for Space Propulsion, Noordwijk, The Netherlands, 20-22 June 2001.

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Abstract

This paper deals with the system-analytical aspects of a high thrust LOX-Kerosene engine to be used in expendable boosters. The attached reference space transportation system is a future Ariane 5 with cryogenic core and upper stage, but skipped solid rocket boosters. The booster engine design is based on a gas generator cycle and features some of the low cost design parameters which were applied to the MC-1 engine. The investigations are focused on the feasibility and the effects of such an engine design when applied to booster propulsion of large launch vehicles such as ARIANE 5.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2001,
Title:Systems Analysis of a High Thrust, Low-Cost Rocket Engine
Authors:
AuthorsInstitution or Email of Authors
Kauffmann, J.UNSPECIFIED
Herbertz, A.UNSPECIFIED
Sippel, M.UNSPECIFIED
Date:2001
Journal or Publication Title:Fourth International Conference on Green Propellants for Space Propulsion
Editors:
EditorsEmail
ESA, DLR, DEGUSSA, CNES, UNSPECIFIED
Status:Published
Event Title:4th International Conference on Green Propellants for Space Propulsion, Noordwijk, The Netherlands, 20-22 June 2001
Organizer:ESTEC
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 13:54

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