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  2. Lockheed Martin F-22 Raptor - Wikipedia

    en.wikipedia.org/wiki/Lockheed_Martin_F-22_Raptor

    The F-22's thrust-to-weight ratio at typical combat weight is nearly at unity in maximum military power and 1.25 in full afterburner. The fixed shoulder-mounted caret inlets are offset from the forward fuselage to divert the turbulent boundary layer and generate oblique shocks with the upper inboard corners to ensure good total pressure ...

  3. Thrust-to-weight ratio - Wikipedia

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

    Thrust-to-weight ratio is a dimensionless ratio of thrust to weight of a ... Lockheed Martin F-22 >1.09 (1.26 with loaded weight and 50% fuel) [14] General Dynamics F-16:

  4. Pratt & Whitney F119 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_F119

    The ATF's increasing weight during development required more thrust to meet the performance requirements; as gross weight grew to 60,000 lb (27,200 kg), the required maximum thrust was increased by 20% to 35,000 lbf (156 kN) class. Pratt & Whitney's design changed to incorporate a 15% larger fan, increasing bypass ratio from 0.25 to 0.30.

  5. Pratt & Whitney F135 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_F135

    Developed from the Pratt & Whitney F119 engine used on the F-22 Raptor, the F135 produces around 28,000 lbf ... Thrust-to-weight ratio: 4.36:1 military thrust, 6.70:1 ...

  6. Pratt & Whitney PW1000G - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_PW1000G

    The PW8000 had an 11:1 bypass ratio (twice that of the V2500), a 40:1 overall pressure ratio, and 13 compressor stages instead of the 22 [4] in the V2500 for similar thrusts. Preliminary development was to end by June 1, the first test for 10 months later, and certification 20 months after, for $400 million.

  7. Pratt & Whitney JT12 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_JT12

    Diameter: 22 in (560 mm) Dry weight: 468 lb (212 kg) Components. Compressor: 9-stage axial compressor; ... Thrust-to-weight ratio: 7.05; See also. Related development.

  8. Supermaneuverability - Wikipedia

    en.wikipedia.org/wiki/Supermaneuverability

    F-22 Raptor, the first U.S. operational supermaneuverable fighter aircraft.It has thrust vectoring and a thrust-to-weight ratio of 1.26 at 50% fuel.. Traditional aircraft maneuvering is accomplished by altering the flow of air passing over the control surfaces of the aircraft—the ailerons, elevators, flaps, air brakes and rudder.

  9. Template:Engine thrust to weight table - Wikipedia

    en.wikipedia.org/wiki/Template:Engine_thrust_to...

    Thrust Thrust-to-weight ratio (kg) (lb) (kN) (lbf) RD-0410 nuclear rocket engine [1] [2] 2,000 4,400 ... Merlin 1D rocket engine, full-thrust version 467 1,030 825