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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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.|
|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|
|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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