A Comparison of Future Fully Reusable Winged Single-stage and Two-stage Launch Vehicles with Different Propulsion Concepts.
Daniel Wolf
Abstract
Daniel Wolf
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.
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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.
Key concepts: Stage (stratigraphy), Single stage, Propulsion, Launch vehicle, Aerospace engineering, Engineering, Ramjet, Automotive engineering