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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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)|
|Title:||Reusable Hydro-Carbon Booster Stages as a Replacement for Large Solid Rocket Motors|
|Journal or Publication Title:||Fourth International Conference on Green Propellants for Space Propulsion|
|Event Title:||4th International Conference on Green Propulsion for Space Propulsion, Noordwijk, The Netherlands|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Space|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||Space|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||E -- no assignement|
|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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