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  2. Concorde - Wikipedia

    en.wikipedia.org/wiki/Concorde

    Nevertheless, soon after Concorde began flying, a Concorde "B" model was designed with slightly larger fuel capacity and slightly larger wings with leading edge slats to improve aerodynamic performance at all speeds, with the objective of expanding the range to reach markets in new regions. [121]

  3. Thrust-specific fuel consumption - Wikipedia

    en.wikipedia.org/wiki/Thrust-specific_fuel...

    For example, Concorde cruised at 1354 mph, or 7.15 million feet per hour, with its engines giving an SFC of 1.195 lb/(lbf·h) (see below); this means the engines transferred 5.98 million foot pounds per pound of fuel (17.9 MJ/kg), equivalent to an SFC of 0.50 lb/(lbf·h) for a subsonic aircraft flying at 570 mph, which would be better than even ...

  4. Thrust-to-weight ratio - Wikipedia

    en.wikipedia.org/wiki/Thrust-to-weight_ratio

    Concorde: 0.372 Max take-off weight, full afterburners Rockwell International B-1 Lancer: 0.38 Max take-off weight, full afterburners HESA Kowsar: 0.61 With full fuel, afterburners. BAE Hawk: 0.65 [9] Lightning F.6: 0.702 Max take-off weight, full afterburners Lockheed Martin F-35 A: 0.87 [citation needed] With full fuel (1.07 with 50% fuel, 1. ...

  5. Fuel economy in aircraft - Wikipedia

    en.wikipedia.org/wiki/Fuel_economy_in_aircraft

    Concorde, a supersonic transport, managed about 17 passenger-miles to the Imperial gallon, which is 16.7 L/100 km per passenger; similar to a business jet, but much worse than a subsonic turbofan aircraft. Airbus states a fuel rate consumption of their A380 at less than 3 L/100 km per passenger (78 passenger-miles per US gallon). [52]

  6. Fuel fraction - Wikipedia

    en.wikipedia.org/wiki/Fuel_fraction

    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]

  7. Chrysler Concorde - Wikipedia

    en.wikipedia.org/wiki/Chrysler_Concorde

    The Chrysler Concorde is a full-size car that was produced by Chrysler from 1992 to 2004. It assumed the C-body Chrysler New Yorker Salon 's position as the entry-level full-size sedan in the Chrysler brand lineup.

  8. List of airliners by maximum takeoff weight - Wikipedia

    en.wikipedia.org/wiki/List_of_airliners_by...

    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

  9. Supersonic transport - Wikipedia

    en.wikipedia.org/wiki/Supersonic_transport

    The Concorde supersonic transport had an ogival delta wing, a slender fuselage and four underslung Rolls-Royce/Snecma Olympus 593 engines. The Tupolev Tu-144 was the first SST to enter service and the first to leave it.