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- W2316982382 abstract "The principal objective of this work is to investigate the conceptual design and perform finite element structural analysis of a hyper-energetic beam-boosted aerospacecraft capable of transporting 12 occupants around the planet (and back), into low Earth orbit, or directly to the Moon without resorting to refueling or staging. As proposed, the double-hull of the 20-m diameter super-pressure balloon-type craft may be constructed from microwave-transparent silicon carbide films of superior strength (i.e., thin films with properties equal to our best carbon fibers), and inflated with helium. The addition of an oxygen partial pressure of 69-mm of Hg, makes this a breathable mixture for the crew. Exotic thin-film and composite fabrication methods are employed to achieve extreme light weight (2400-kg) and structural stability. The lenticular spacecraft design is dominated by the magnetohydrodynamic (MHD) propulsion system geometry, and by human factors requirements. The remote beamenergized MHD powerplant is intimately integrated with the crafts tensile-type structure, and is not distinguishable as an item separate from the vehicle as in conventional aircraft. The design assumption of liquid immersion G-suits, partial liquid ventilation, and individualized escape" @default.
- W2316982382 created "2016-06-24" @default.
- W2316982382 creator A5049951014 @default.
- W2316982382 creator A5076667686 @default.
- W2316982382 date "1998-07-13" @default.
- W2316982382 modified "2023-09-28" @default.
- W2316982382 title "Three dimensional transient structural analysis of a transatmospheric beam-boosted, super-pressure aerospacecraft" @default.
- W2316982382 cites W2164884913 @default.
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- W2316982382 doi "https://doi.org/10.2514/6.1998-3742" @default.
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