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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.

Full text not available from this repository.

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.

Item URL in elib:https://elib.dlr.de/1522/
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 AuthorsAuthors ORCID iD
Kauffmann, J.UNSPECIFIEDUNSPECIFIED
Herbertz, A.UNSPECIFIEDUNSPECIFIED
Sippel, M.UNSPECIFIEDUNSPECIFIED
Date:2001
Journal or Publication Title:Fourth International Conference on Green Propellants for Space Propulsion
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
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 assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Lohmiller, Monika
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:54

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