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  2. Ayres Thrush - Wikipedia

    en.wikipedia.org/wiki/Ayres_Thrush

    The Ayres Thrush, formerly the Snow S-2, [1] Aero Commander Ag Commander, and Rockwell Thrush Commander, is an American agricultural aircraft produced by Ayres Corporation and more recently by Thrush Aircraft. It is one of the most successful and long-lived agricultural application aircraft types in the world, with almost 2,000 sold since the ...

  3. SpaceX Raptor - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Raptor

    It featured 200 bars (20 MPa; 2,900 psi) of chamber pressure, with a thrust of 1 meganewton (220,000 lb f) and used the SpaceX-designed SX500 alloy, created to contain hot oxygen gas in the engine at up to 12,000 pounds per square inch (830 bar; 83 MPa). [35] It was tested on a ground test stand in McGregor, firing briefly. [21]

  4. RS-25 - Wikipedia

    en.wikipedia.org/wiki/RS-25

    The RS-25 engine consists of pumps, valves, and other components working in concert to produce thrust. Fuel (liquid hydrogen) and oxidizer (liquid oxygen) from the Space Shuttle's external tank entered the orbiter at the umbilical disconnect valves and from there flowed through the orbiter's main propulsion system (MPS) feed lines; whereas in the Space Launch System (SLS), fuel and oxidizer ...

  5. M35 series 2½-ton 6×6 cargo truck - Wikipedia

    en.wikipedia.org/wiki/M35_series_2½-ton_6×6...

    The turbo was added more to clean up the black exhaust on the Non Turbo engines, than to add power; the HP was raised from 130 to only 135 HP. Turbo models used: 3LD305 (early engines only) and 3LJ319 (the "whistler") The LDT-465-1D was the last version of the Multi Fuel, it had the same 3LJ319 Turbo (whistler), or the quieter 3LM39 (non ...

  6. Jet engine - Wikipedia

    en.wikipedia.org/wiki/Jet_engine

    Jet engine during take-off showing visible hot exhaust (Germanwings Airbus A319)A jet engine is a type of reaction engine, discharging a fast-moving jet of heated gas (usually air) that generates thrust by jet propulsion.

  7. Saturn V - Wikipedia

    en.wikipedia.org/wiki/Saturn_V

    The engine exhaust from the S-II stage glows as it impacts the interstage. After S-IC separation, the S-II second stage burned for 6 minutes and propelled the craft to 109 miles (175 km) and 15,647 mph (25,181 km/h), close to orbital velocity .

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