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

Daniel Wolf

Open publisher page 2 citations

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.

About this research paper

What this paper is about

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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OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available 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.

Key concepts: Stage (stratigraphy), Single stage, Propulsion, Launch vehicle, Aerospace engineering, Engineering, Ramjet, Automotive engineering

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A Comparison of Future Fully Reusable Winged Single-stage and Two-stage Launch Vehicles with Different Propulsion Concepts. — Research Paper | ScholarLens