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- W2321832114 abstract "Trajectory simulations from Earth to orbit indicate comparative velocity requirements depending on vehicle size, for several propellant options. Smaller vehicles are more affected by drag, resulting in steeper trajectories that require more total velocity. Although they are technically challenging, launch vehicles smaller than 1 ton are not ruled out by the nature of ascent trajectories." @default.
- W2321832114 created "2016-06-24" @default.
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- W2321832114 date "2005-07-10" @default.
- W2321832114 modified "2023-09-24" @default.
- W2321832114 title "How Small Can a Launch Vehicle Be?" @default.
- W2321832114 doi "https://doi.org/10.2514/6.2005-4506" @default.
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