A conceptual study of high speed rotorcraft

dc.contributor.author Tanabe, Y.
dc.contributor.author Aoyama, T.
dc.contributor.author Kobiki, N.
dc.contributor.author Sugiura, M.
dc.contributor.author Miyashita, R.
dc.contributor.author Sunada, S.
dc.contributor.author Kawachi, K.
dc.contributor.author Nagao, M.
dc.date.accessioned 2016-12-16T15:14:39Z
dc.date.available 2016-12-16T15:14:39Z
dc.date.issued 2014
dc.description.abstract A 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.other 33-B-paper
dc.identifier.uri http://hdl.handle.net/20.500.11881/3501
dc.language.iso en
dc.title A conceptual study of high speed rotorcraft
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