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- W2321819911 abstract "Considered are the possibilities of using a rocket-powered reusable winged hypersonic module as an ascent stage with various types of start. The configuration of the module was defined and its main parameters were optimized for each start type. The payload mass, relative mass and dry mass were used as criteria for comparison. The orbit insertion trajectories were computed with using approximately optimal control laws. A comparison with a precise solution by using the Pontrjagin’s maximum principle is given. Some considerations concerning module unification for several types of start and stage unification of two-stage space system with vertical start are stated." @default.
- W2321819911 created "2016-06-24" @default.
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- W2321819911 date "2003-09-29" @default.
- W2321819911 modified "2023-09-25" @default.
- W2321819911 title "Comparison of Reusable Space Transportation Systems with Different Types of Start and Assessment of the Possibility of their Unification on the Basis of a Winged Module" @default.
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- W2321819911 doi "https://doi.org/10.2514/6.iac-03-v.p.07" @default.
- W2321819911 hasPublicationYear "2003" @default.
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