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A Comparison of Future Fully Reusable Winged Single-stage and Two-stage Launch Vehicles with Different Propulsion Concepts.

Wolf, D. M. (1990) A Comparison of Future Fully Reusable Winged Single-stage and Two-stage Launch Vehicles with Different Propulsion Concepts. 41st Congress of the IAF, 6-12 October 1990, Dresden.

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Abstract

The paper deals with the evaluation of future fully reusable launch vehicles on the basis of mass and cost comparisons. 16 winged single- stage and two-stage vehicles are compared. It is found that neither the horizontal take-off single-stage vehicles nor the single-stage ramjet vehicles represent an alternative to the vertical take-off single-stage rocket vehicles.

Document Type:Conference or Workshop Item (Speech)
Additional Information: LIDO-Berichtsjahr=1990, pages=6,
Title:A Comparison of Future Fully Reusable Winged Single-stage and Two-stage Launch Vehicles with Different Propulsion Concepts.
Authors:
AuthorsInstitution or Email of Authors
Wolf, D. M.UNSPECIFIED
Date:1990
Status:Published
Keywords:Launch Vehicle, Propulsion Concept
Event Title:41st Congress of the IAF, 6-12 October 1990, Dresden
HGF - Research field:UNSPECIFIED
HGF - Program:other
HGF - Program Themes:other
DLR - Research area:UNSPECIFIED
DLR - Program:no assignment
DLR - Research theme (Project):UNSPECIFIED
Location: Köln-Porz
Institutes and Institutions:Institute of Transport Research > Hauptabteilung Systemanalyse Raumfahrt
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:05

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