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Its wing has a span of 33 ft (10.1 m), wing area is 195 sq ft (18.1 m 2) and the aspect ratio is 5.6:1. The pilot hook-in weight range is 175 to 275 lb (79 to 125 kg). Improvements over the Falcon 3 include a new sail cut and layout, improved lateral stability at higher speeds and under aero towing and an optional Litestream control bar. [2]
Dassault launched the FNX at the 2001 Paris Air Show, aiming for a 10,500km (5,700nm) range at Mach 0.88, up from the Falcon 900EX's 8,300 km at Mach 0.84. Its new high-speed wing is 1.86 m (6 ft 1 in) longer with 5° higher wing sweep than the 900 wing; while its fuselage is 20% longer, it keeps the same cabin cross-section but with a new curved windscreen.
The Dassault Falcon 50 is a French super-midsize, long-range business jet, featuring a trijet layout with an S-duct air intake for the central engine. It has the same fuselage cross-section and similar capacity as the earlier twin-engined Falcon 20, but was a new design that is area ruled and includes a more advanced wing design.
Created Date: 8/30/2012 4:52:52 PM
The Falcon 6X reinforces the 5X new 70.7 m 2 (761 sq ft) wing and keeps its digital flight control system and Honeywell Primus Epic EASy III flight deck. The new engine fans have a diameter of 110 cm (44 in), 15 cm (6 in) narrower than the Gulfstreams, with four low-pressure turbine stages instead of five, engine weight is reduced by 91 kg (200 ...
The straight-through layout leaves the engine high above the ground, making access difficult. The straight-through layout also increases total aerodynamic drag by 2–4%. [1] Compared to the straight-through design on the DC-10 and MD-11, the S-duct allows a shorter fin and a rudder closer to the longitudinal axis.
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It is 33.4 m (110 ft) long and has a 33.6 m (110 ft)-wide, high aspect ratio carbonfibre wing, a first for a Dassault business jet. [1] It is powered by two Rolls-Royce Pearl 10X engines with over 80 kN (18,000 lbf) thrust, with a titanium fan blisk, a 10-stage HP compressor, a two-stage shroudless HP turbine and a four-stage LP turbine. [1]
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