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  2. 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 ...

  3. Template:Jetspecs - Wikipedia

    en.wikipedia.org/wiki/Template:Jetspecs

    This template employs intricate features of template syntax. You are encouraged to familiarise yourself with its setup and parser functions before editing the template. If your edit causes unexpected problems, please undo it quickly, as this template may appear on a large number of pages.

  4. Propelling nozzle - Wikipedia

    en.wikipedia.org/wiki/Propelling_nozzle

    Afterburner-equipped engines may also open the nozzle for starting and at idle. The idle thrust is reduced which lowers taxi speeds and brake wear. This feature on the J75 engine in the F-106 was called 'Idle Thrust Control' and reduced idle thrust by 40%. [28] On aircraft carriers, lower idle thrust reduces the hazards from jet blast.

  5. Thrust vectoring - Wikipedia

    en.wikipedia.org/wiki/Thrust_vectoring

    A multi-axis thrust vectoring engine nozzle in motion. Thrust vectoring, also known as thrust vector control (TVC), is the ability of an aircraft, rocket or other vehicle to manipulate the direction of the thrust from its engine(s) or motor(s) to control the attitude or angular velocity of the vehicle.

  6. Pulsejet - Wikipedia

    en.wikipedia.org/wiki/Pulsejet

    A pulsejet engine (or pulse jet) is a type of jet engine in which combustion occurs in pulses.A pulsejet engine can be made with few [1] or no moving parts, [2] [3] [4] and is capable of running statically (that is, it does not need to have air forced into its inlet, typically by forward motion).

  7. Gas turbine engine thrust - Wikipedia

    en.wikipedia.org/wiki/Gas_turbine_engine_thrust

    The familiar study of jet aircraft treats jet thrust with a "black box" description which only looks at what goes into the jet engine, air and fuel, and what comes out, exhaust gas and an unbalanced force. This force, called thrust, is the sum of the momentum difference between entry and exit and any unbalanced pressure force between entry and ...

  8. Gulfstream G280 - Wikipedia

    en.wikipedia.org/wiki/Gulfstream_G280

    Data from Gulfstream General characteristics Crew: 2 Capacity: seating for 10 in executive style and 4,050 pounds (1,840 kg) payload Length: 66 ft 10 in (20.3 m) Wingspan: 63 ft 0 in (19.2 m) Height: 21 ft 4 in (6.5 m) Wing area: 495 sq ft (46 m 2) Empty weight: 24,150 lb (10,954 kg) Max takeoff weight: 39,600 lb (17,960 kg) Powerplant: 2 × Honeywell HTF7250G turbofans, 7,624 lbf (33.91 kN ...

  9. Target-type thrust reversal - Wikipedia

    en.wikipedia.org/wiki/Target-type_thrust_reversal

    Video of a target-type thrust reverser in operation. Target-type thrust reversal (also called bucket thrust reversal or clamshell thrust reversal [1]) is a deceleration method when an aircraft lands. Like other types of thrust reversals, it temporarily diverts the engine exhaust forward to provide deceleration. This type of thrust-reverser is ...