A conceptual study of high speed rotorcraft

dc.contributor.authorTanabe, Y.
dc.contributor.authorAoyama, T.
dc.contributor.authorKobiki, N.
dc.contributor.authorSugiura, M.
dc.contributor.authorMiyashita, R.
dc.contributor.authorSunada, S.
dc.contributor.authorKawachi, K.
dc.contributor.authorNagao, M.
dc.date.accessioned2016-12-16T15:14:39Z
dc.date.available2016-12-16T15:14:39Z
dc.date.issued2014
dc.description.abstractA study group of future rotorcraft is formed in JAXA with participants from a wide spectra of organizations in Japan. Taking the helicopter market in Japan as a study case, four potential high speed rotorcraft (VTOL aircraft) missions are discussed. When a capability of hovering is required, compound helicopter is concluded as the most suitable design configuration. A simplified conceptual design process for a compound helicopter is described where a wing and propellers are added to a single rotor helicopter. A compound helicopter concept for high speed EMS (Emergency Medical Service) is proposed. The result of the conceptual design is compared with a conventional helicopter and the cost expense is illustrated. If also considering the cost to maintain a base hospital, a high speed rotorcraft with significant higher cost is acceptable which covers a much wider area providing effective first aid to critical patients
dc.identifier.other33-B-paper
dc.identifier.urihttp://hdl.handle.net/20.500.11881/3501
dc.language.isoen
dc.titleA conceptual study of high speed rotorcraft

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