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  2. Rocket engine nozzle - Wikipedia

    en.wikipedia.org/wiki/Rocket_engine_nozzle

    The ratio of the area of the narrowest part of the nozzle to the exit plane area is mainly what determines how efficiently the expansion of the exhaust gases is converted into linear velocity, the exhaust velocity, and therefore the thrust of the rocket engine. The gas properties have an effect as well.

  3. Nozzle extension - Wikipedia

    en.wikipedia.org/wiki/Nozzle_extension

    A nozzle extension is an extension of the nozzle of a reaction/rocket engine. The application of nozzle extensions improves the efficiency of rocket engines in vacuum by increasing the nozzle expansion ratio.

  4. Rocket engine - Wikipedia

    en.wikipedia.org/wiki/Rocket_engine

    The four expansion regimes of a de Laval nozzle: • under-expanded • perfectly expanded • over-expanded • grossly over-expanded. The most commonly used nozzle is the de Laval nozzle, a fixed geometry nozzle with a high expansion-ratio. The large bell- or cone-shaped nozzle extension beyond the throat gives the rocket engine its ...

  5. Expanding nozzle - Wikipedia

    en.wikipedia.org/wiki/Expanding_nozzle

    The expanding nozzle is a type of rocket nozzle that, unlike traditional designs, maintains its efficiency at a wide range of altitudes. It is a member of the class of altitude compensating nozzles, a class that also includes the plug nozzle and aerospike. While the expanding nozzle is the least technically advanced and simplest to understand ...

  6. Expansion deflection nozzle - Wikipedia

    en.wikipedia.org/wiki/Expansion_deflection_nozzle

    The expansion-deflection nozzle is a rocket nozzle which achieves ... the atmospheric pressure affects the exit area ratio so that atmospheric compensation can be ...

  7. Bell nozzle - Wikipedia

    en.wikipedia.org/wiki/Bell_nozzle

    The bell-shaped or contour nozzle is probably the most commonly used shaped rocket engine nozzle. It has a high angle expansion section (20 to 50 degrees) right behind the nozzle throat; this is followed by a gradual reversal of nozzle contour slope so that at the nozzle exit the divergence angle is small, usually less than a 10 degree half angle.

  8. RL10 - Wikipedia

    en.wikipedia.org/wiki/RL10

    The RL10 was the first liquid hydrogen rocket engine to be built in the United States, ... Nozzle expansion ratio: 40 to 1; Propellant flow: 35 lb/s (16 kg/s)

  9. RS-25 - Wikipedia

    en.wikipedia.org/wiki/RS-25

    The nozzle is a bell-shaped extension bolted to the main combustion chamber, referred to as a de Laval nozzle. The RS-25 nozzle has an unusually large expansion ratio (about 69:1) for the chamber pressure. [12]