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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.

Full text not available from this repository.

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.

Item URL in elib:https://elib.dlr.de/22995/
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 AuthorsAuthors ORCID iD
Wolf, D. M.UNSPECIFIEDUNSPECIFIED
Date:1990
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
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: DLR-Beauftragter, elib
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:05

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