EuroFAR

European Future Advanced Rotorcraft (EuroFAR) was a proposed tiltrotor passenger aircraft that was developed beginning in Template:Avyear until it was abandoned in the late 1990s. The project was initiated by a European consortium that included Aerospatiale, Agusta, Messerschmitt-Bölkow-Blohm (MBB), Westland, Aeritalia, and Construcciones Aeronáuticas SA (CASA).

Specifications

Data from Future Aeronautical and Space Systems (1997), pp. 62, 65

General characteristics

• Crew: 2 pilots, 1 flight attendant
• Capacity: 30 passengers
• Length: 22.4 m (73 ft 6 in)
• Wingspan: 14.6 m (47 ft 11 in)
• Max takeoff weight: 15,000 kg (33,069 lb) VTOL: 13,650 kg (30,090 lb)
• Powerplant: 2 × Pratt & Whitney PW300 turboshaft, 3,185 kW (4,271 hp) each
• Main rotor diameter: × 11.2 m (36 ft 9 in)

Performance

• Cruise speed: 620 km/h (386 mph, 335 kn)
• Range: 1,230 km (764 mi, 664 nmi) with maximum standard fuel
• Rate of climb: 11 m/s (2,200 ft/min)

See also

• AgustaWestland AW609
• Bell Boeing V-22 Osprey

Bibliography

• "Eurofar renews work on tilt-rotor programme". Flight International. 12 November 1997. p. 32. ISSN 0015-3710.
• "Europeans plan civil tiltrotor technology demonstrator". Helicopter News. Vol. 22, no. 5. 1 March 1996. p. 1. ISSN 0363-8227 – via Factiva.
• "Pressured by U.S. efforts, EuroFAR picks up speed". Helicopter News. Vol. 21, no. 16. 4 August 1995. p. 1. ISSN 0363-8227 – via Factiva.
• Richard, Yves (February 1995). Eurocopter France head outlines R&D program. Aerospace. Science & Technology: Europe/International (Report). JPRS Report. Vol. JPRS-EST-95-014. Translated by Foreign Broadcast Information Service (FBIS) (published 22 May 1995). pp. 3–9. hdl:2027/nyp.33433016823936. {{cite report}}: Unknown parameter |agency= ignored (help)
• Martini, A.; Renaud, J. (24–27 May 1993). Le convertible type EuroFAR: Vue d'ensemble des avancements techniques et missions futures (PDF). Recent advances in long range and long endurance operation of aircraft. Flight Mechanics Panel Symposium. AGARD conference proceedings (in French). Vol. 547. Kijkduin (The Hague), Netherlands: North Atlantic Treaty Organization (NATO) (published November 1993). pp. 10–1 to 10–6. ISBN 92-835-0726-6. ISSN 0549-7191. OCLC 197117575.
• Tardif, Christel (1–7 March 1993). Technical features of EUROFAR VTOL aircraft described. West Europe: Aerospace. Science & Technology: Europe/International (Report). JPRS Report. Vol. JPRS-EST-93-010-L. Translated by Foreign Broadcast Information Service (FBIS) (published 16 April 1993). pp. 12–13. hdl:2027/nyp.33433017047170. {{cite report}}: Unknown parameter |agency= ignored (help)
• Tardif, Christel (18–24 January 1993). EUROFAR enters demonstrator phase. West Europe: Aerospace. Science & Technology: Europe/International (Report). JPRS Report. Vol. JPRS-EST-93-006-L. Translated by Foreign Broadcast Information Service (FBIS) (published 22 February 1993). pp. 3–4. hdl:2027/nyp.33433017047170. {{cite report}}: Unknown parameter |agency= ignored (help)
• Renaud, J.; Huber, H.; Venn, G. (24–27 September 1991). The EuroFAR program: An European overview on advanced VTOL civil transportation system (PDF). European rotorcraft forum (17th ed.). Berlin, Germany. hdl:20.500.11881/3387. OCLC 256210503.
• Gavaghan, Helen (1 October 1987). "Tilting at new aviation markets. In the US, the armed forces will soon operate aircraft that take off and land as helicopters but fly like turboprops. Europe is now beginning to take an interest in the technology for a civilian market". New Scientist. Vol. 116, no. 1580. pp. 38–43. ISSN 0028-6664.
• Andres, J.; Huber, H.; Renaud, J. (22–25 September 1986). The tilt-rotor aircraft: A response to the future? From European interrogations to EuroFAR actions (PDF). European rotorcraft forum (12th ed.). Garmisch-Partenkirchen, Germany. hdl:20.500.11881/2983. OCLC 256382680.