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Template: Engine thrust to weight table. 1 language. ... RD-0410 nuclear rocket engine [1] [2] 2,000 4,400 35.2 7,900 1.8 J58 jet engine (SR-71 Blackbird) [3] [4] 2,722
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]
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
Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389
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 ...
With a fuel fraction of nearly 85%, the GlobalFlyer could carry 5 times its weight in fuel.. In aerospace engineering, an aircraft's fuel fraction, fuel weight fraction, [1] or a spacecraft's propellant fraction, is the weight of the fuel or propellant divided by the gross take-off weight of the craft (including propellant): [2]
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)
Single-engined tractor aircraft (1 C, 4,830 P) Single-engined turboprop aircraft (134 P) This page was last ... Category: Single-engine aircraft.