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A new wing root section would lengthen its span by 3.8 ft (1.2 m) to 41.7 ft (12.7 m), which would increase the wing area to 163 sq ft (15.1 m 2), 13% more, and eliminate the tip tanks to reduce drag. 70 US gal (260 L) more fuel could be carried to reach 321 US gal (1,220 L), and a higher MTOW would increase the useful load to 2,787 lb (1,264 ...
Its FJ44 engine has a 16:1 overall pressure ratio and a 2.58:1 bypass ratio. [ 8 ] [ 11 ] Early CitationJet models have a novel design feature to reduce weight: rather than conventional thrust reversers , the aircraft are equipped with thrust attenuator paddles that pivot from the rear fuselage, similar to those used on the Cessna T-37 Tweet ...
The conversion cost $1.9 million in 2009, resulting in a $3.5-4.6 million value for a converted Citation II. [18] Ceiling is increased from FL 410 to FL 430, reached directly in 25 min at max takeoff weight with a thrust increased from 2,500 to 2,820 lbf (11.1 to 12.5 kN) each. [18]
1.8 J58 jet engine (SR-71 Blackbird) [3] [4] 2,722 6,001 150 34,000 5.2 Rolls-Royce/Snecma Olympus 593 ... Template: Engine thrust to weight table.
Type MTOW [kg] MLW [tonnes] TOR [m] LR [m] ICAO category FAA category; Antonov An-225: 640,000: 591.7: 3,500: Super: Super Scaled Composites Model 351 Stratolaunch
Research into the next generation of commercial jet engines, high-bypass ratio turbofans in the "10-ton" (20,000 lbf; 89 kN) thrust class, began in the late 1960s. Snecma (now Safran), who had mostly built military engines previously, was the first company to seek entrance into the market by searching for a partner with commercial experience to design and build an engine in this class.
The Cessna Skymaster is an American twin-engine civil utility aircraft built in a push-pull configuration. ... Empty weight: 2,655 lb (1,204 kg)
Cessna Citation Mustang instrument panel A Mustang PW615F engine uncowled. Data from Cessna Aircraft Company [14] General characteristics. Crew: one or two pilots; Capacity: 4 to 5 passengers and 3130 lb (1420 kg) useful load; Length: 40 ft 7 in (12.37 m) Wingspan: 43 ft 2 in (13.16 m) Height: 13 ft 5 in (4.09 m) Empty weight: 5,600 lb (2,540 kg)