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Reusable Hydro-Carbon Booster Stages as a Replacement for Large Solid Rocket Motors

Sippel, M. and Atanassov, U. and Kauffmann, J. and Klevanski, J. and Schmid, V. (2001) Reusable Hydro-Carbon Booster Stages as a Replacement for Large Solid Rocket Motors. In: Fourth International Conference on Green Propellants for Space Propulsion. 4th International Conference on Green Propulsion for Space Propulsion, Noordwijk, The Netherlands.

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Abstract

This paper investigates different types of reusable first stages using hydro-carbon propulsion designed for a near term application with heavy lift launchers. The attached reference expendable space transportation system is a future Ariane 5 with cryogenic core and upper stage, but skipped solid rocket boosters. The design of the so called liquid fly-back boosters (LFBB) is restricted here to the incorporation of hydro-carbon-LOX rocket motors already under developmnt or in operation.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2001,
Title:Reusable Hydro-Carbon Booster Stages as a Replacement for Large Solid Rocket Motors
Authors:
AuthorsInstitution or Email of Authors
Sippel, M.UNSPECIFIED
Atanassov, U.UNSPECIFIED
Kauffmann, J.UNSPECIFIED
Klevanski, J.UNSPECIFIED
Schmid, V.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 Propulsion for Space Propulsion, Noordwijk, The Netherlands
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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