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| JR TU-414 Superior business jet |
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| FS2004/FSX | |
| JRLucariny FSDS V3.5 Model | |
| Download/DonationWare | |
| Set/2007 | |
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| JR TU-414 Superior business jet |
|
| FS2004/FSX | |
| JRLucariny FSDS V3.5 Model | |
| Download/DonationWare | |
| Set/2007 | |
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TUPOLEV TU-414 |
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The sheer size of the former Soviet Union prompted ANTK Tupolev to study a superior business jet with exceptional range. |
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The Tu-414 was announced in 1994. |
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Like the other recent projects, the basic features can be seen in the drawing. |
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Diameter of the highly pressurised fuselage would be 2.5m (98.4in), and the selected engine is the BMW Rolls-Royce BR 710, rated at 14,9901b. |
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Passenger capacity could be from eight to nineteen in the executive role, or thirty as a regional transport (though the long range fits it for very long 'thin' routes). |
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The long range results in greater sweepback than on the 204 and 334, the wing leading edge being set at 33 deg. |
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ANTK Tupolev hopes to receive funds from a national programme to support civil aviation for year 2000. |
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TUPOLEV TU-414 JRLucariny Panel Model |
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Span 28.8m (94ft 51/8in); Length 28.2m (92ft 6 1\4in); |
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Maximum payload 3,300kg (7,275111); maximum take-off weight 10,000Kg (88, 183lb); Cruising speed 860km/h (534mph); |
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Range 10,560km (6,562 miles) with passengers, 8,500km (5,282 miles) with 30 passengers; Required runway length 2,040m (6,692ft). Font: PUTNAM – “TUPOLEV AIRCRAFT since1922” Bill Gunston |
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TUPOLEV TU-414 |
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DRAWINGS |