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Progress in the Design of a Reusable Launch Vehicle Stage

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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Abstract

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
Authors:
AuthorsInstitution or Email of Authors
Sippel, M.UNSPECIFIED
Klevanski, J.UNSPECIFIED
Burkhardt, H.UNSPECIFIED
Date:2002
Journal or Publication Title:38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Editors:
EditorsEmail
American Institute of Aeronautics and Astronautics, UNSPECIFIED
Publisher:AIAA
Status:Published
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
Location: Lampoldshausen
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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