Sippel, M. and Klevanski, J. and Burkhardt, H. (2002) Progress in the Design of a Reusable Launch Vehicle Stage. In: 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. AIAA. 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN, 7 - 10 July 2002.
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The German future launcher technology research program ASTRA investigates in its system study two types of partially reusable launch vehicles. This paper describes one of those concepts, a reusable first stage designed for a near term application with a heavy lift launcher. 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 reference liquid fly-back boosters (LFBB) is focused on LOX/LH2 propellant and a future derivative of the Vulcain rocket motor.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=2002, monograph_id=AIAA 2002-5220,|
|Title:||Progress in the Design of a Reusable Launch Vehicle Stage|
|Journal or Publication Title:||38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference|
|Event Title:||38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, IN, 7 - 10 July 2002|
|Organizer:||American Institute of Aeronautics and Astronautics|
|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|
|Institutes and Institutions:||Institute of Space Propulsion|
|Deposited By:||Monika Lohmiller|
|Deposited On:||16 Sep 2005|
|Last Modified:||06 Jan 2010 13:59|
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