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  2. K&N Engineering - Wikipedia

    en.wikipedia.org/wiki/K&N_Engineering

    K&N Engineering, Inc. (also known simply as K&N) is a manufacturer of air filters, cold air intake systems, oil filters, performance parts, and other related products. [1] K&N manufactures over 12,000 parts for various makes and models of cars, trucks, SUVs, motorcycles, ATVs, industrial applications and more.

  3. Multi-valve - Wikipedia

    en.wikipedia.org/wiki/Multi-valve

    A cylinder head of a four valve Nissan VQ engine engine. A multi-valve or multivalve engine is one where each cylinder has more than two valves (an intake, and an exhaust).A multi-valve engine has better breathing, and with more smaller valves (having less mass in motion) may be able to operate at higher revolutions per minute (RPM) than a two-valve engine, delivering more power.

  4. Staged combustion cycle - Wikipedia

    en.wikipedia.org/wiki/Staged_combustion_cycle

    Oxidizer-rich turbine exhaust from a SpaceX Raptor preburner shown during a 2015 sub-system test on a test stand at Stennis Space Center. In the full-flow rocket engine, the preburner exhaust is fed into a turbine and then into the main combustion chamber. Several variants of the staged combustion cycle exist.

  5. Briggs & Stratton - Wikipedia

    en.wikipedia.org/wiki/Briggs_&_Stratton

    Designated by an "R" after the basic model, then a 2, 4, or 6 to designate the reduction ratio. high speed models (higher intake capacity to run higher rpm) available on the A B K M R and Z series. designated with an "H" after the basic model. lightweight models (some aluminum parts to save weight) available on the A B I K R and Z series.

  6. Jet engine - Wikipedia

    en.wikipedia.org/wiki/Jet_engine

    = the mass rate of intake air that flows to the core engine ṁ f = the mass rate of intake air that bypasses the core engine v f = the velocity of the air flow bypassed around the core engine v he = the velocity of the hot exhaust gas from the core engine v o = the velocity of the total air intake = the true airspeed of the aircraft BPR ...

  7. S-75 Dvina - Wikipedia

    en.wikipedia.org/wiki/S-75_Dvina

    The S-75 (Russian: С-75; NATO reporting name SA-2 Guideline) is a Soviet-designed, high-altitude air defence system. It is built around a surface-to-air missile with command guidance. Following its first deployment in 1957 it became one of the most widely deployed air defence systems in history.

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