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  2. File:Brayton Cycle TS Afterburner.svg - Wikipedia

    en.wikipedia.org/wiki/File:Brayton_Cycle_TS...

    English: Brayton-Joule cycle diagram (continuous line for ideal cycle, dotted line for real cycle) of a jet aircraft engine with afterburner with engine stations. 1 Inlet 2 Air Intake/Compressor 3 Compressor/Combustion Chamber 4 Combustion Chamber/Turbine 5 Turbine/Afterburner 6 Afterburner/Nozzle

  3. Afterburner - Wikipedia

    en.wikipedia.org/wiki/Afterburner

    A jet engine afterburner is an extended exhaust section containing extra fuel injectors. Since the jet engine upstream (i.e., before the turbine) will use little of the oxygen it ingests, additional fuel can be burned after the gas flow has left the turbines. When the afterburner is turned on, fuel is injected and igniters are fired.

  4. Components of jet engines - Wikipedia

    en.wikipedia.org/wiki/Components_of_jet_engines

    Diagram of a typical gas turbine jet engine. Air is compressed by the compressor blades as it enters the engine, and it is mixed and burned with fuel in the combustion section. The hot exhaust gases provide forward thrust and turn the turbines which drive the compressor blades. 1. Intake 2. Low pressure compression 3. High pressure compression ...

  5. 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.

  6. Tumansky R-25 - Wikipedia

    en.wikipedia.org/wiki/Tumansky_R-25

    An unusual addition to the R-25 was an emergency mode thrust boost which increased the compressor speed to 106% and also increased the afterburner fuel flow with the addition of a second afterburner fuel pump. Thrust was increased to 96.5 kilonewtons (21,700 lb f) below an altitude of 2,000 metres (6,600 ft). The time limit for its use was 1 ...

  7. Tumansky R-15 - Wikipedia

    en.wikipedia.org/wiki/Tumansky_R-15

    The maximum thrust was 7,500 kilograms force (73.5 kN, 16,500 lbf) dry and 11,200 kilograms force (110 kN, 24,700 lbf) with afterburner. This thrust enabled the Mikoyan-Gurevich MiG-25, with two engines, to reach Mach 3.2, although the engines had to be scrapped after a flight to Mach 3.2. The engine had a very high fuel consumption, especially ...

  8. TaylorMade - Wikipedia

    en.wikipedia.org/wiki/TaylorMade

    TaylorMade Golf Company is an American sports equipment manufacturing company based in Carlsbad, California, United States. The company focuses on the golf equipment market, producing golf clubs, balls, and clothing. TaylorMade Golf is currently a subsidiary of Centroid Investment Partners after it was purchased from KPS Capital Partners in May ...

  9. Westinghouse J40 - Wikipedia

    en.wikipedia.org/wiki/Westinghouse_J40

    The J40-8 was only a little over 40 inches (1,000 mm) in diameter but 25 feet (7.6 m) long, with accessories and including the afterburner. It weighed almost 3,500 pounds (1,600 kg), the -6 being almost 7 feet (2.1 m) shorter and about 600 pounds (270 kg) lighter, because it did not have an afterburner.

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