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  2. Afterburner - Wikipedia

    en.wikipedia.org/wiki/Afterburner

    Since the afterburning exit temperature is effectively fixed, [why?] the temperature rise across the unit increases, raising the afterburner fuel flow. The total fuel flow tends to increase faster than the net thrust, resulting in a higher specific fuel consumption (SFC). However, the corresponding dry power SFC improves (i.e. lower specific ...

  3. General Electric F101 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_F101

    Specific fuel consumption: 0.562 lb/lbf/h (57.3 kg/kN/h) (dry thrust), 2.46 lb/lbf/h (251 kg/kN/h) (with afterburner) Thrust-to-weight ratio : 7.04:1 (afterburner)

  4. Pratt & Whitney F119 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_F119

    The three-zone (reduced from four from the prototype) afterburner, or augmentor, contributes to the stealth of the aircraft by having fuel injectors integrated into thick curved vanes coated with ceramic radar-absorbent materials (RAM). These vanes replace the traditional fuel spray bars and flame holders and block line-of-sight of the turbines.

  5. Pratt & Whitney F135 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_F135

    The Pratt & Whitney F135 is an afterburning turbofan developed for the Lockheed Martin F-35 Lightning II, a single-engine strike fighter.It has two variants; a Conventional Take-Off and Landing variant used in the F-35A and F-35C, and a two-cycle Short Take-Off Vertical Landing variant used in the F-35B that includes a forward lift fan. [1]

  6. Pratt & Whitney J58 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_J58

    The Pratt & Whitney J58 (company designation JT11D-20) is an American jet engine that powered the Lockheed A-12, and subsequently the YF-12 and the SR-71 aircraft. It was an afterburning turbojet engine with a unique compressor bleed to the afterburner that gave increased thrust at high speeds.

  7. Pratt & Whitney TF30 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_TF30

    It was later adapted with an afterburner for supersonic designs, and in this form it was the world's first production afterburning turbofan, going on to power the F-111 and the F-14A Tomcat, as well as being used in early versions of the A-7 Corsair II without an afterburner. First flight of the TF30 was in 1964 and production continued until 1986.

  8. General Electric J85 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_J85

    It features an eight-stage axial-flow compressor powered by two turbine stages, and is capable of generating up to 2,100 lb f (9.3 kN) of dry thrust, or more with an afterburner. At full throttle at sea level, this engine, without afterburner, consumes approximately 400 US gallons (1,500 L) of fuel per hour.

  9. Pratt & Whitney J57 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_J57

    Pratt & Whitney designed the J57 to have a relatively high overall pressure ratio to help improve both thrust-specific fuel consumption and specific thrust, but it was known that throttling a single high-pressure-ratio compressor would cause

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