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  2. 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.

  3. Rocket engine nozzle - Wikipedia

    en.wikipedia.org/wiki/Rocket_engine_nozzle

    The optimal size of a rocket engine nozzle is achieved when the exit pressure equals ambient (atmospheric) pressure, which decreases with increasing altitude. The reason for this is as follows: using a quasi-one-dimensional approximation of the flow, if ambient pressure is higher than the exit pressure, it decreases the net thrust produced by ...

  4. Oil burner - Wikipedia

    en.wikipedia.org/wiki/Oil_burner

    To set the heat output of the burner, the rate of fuel delivery via the nozzle must be adjustable. This is often achieved by an adjustable pressure relief valve between the pump and the nozzle. When the set pressure is reached (usually 100 psi), this valve opens and allows excess oil to flow through a bypass back to the fuel tank or the pump ...

  5. Propelling nozzle - Wikipedia

    en.wikipedia.org/wiki/Propelling_nozzle

    Overexpansion occurs when the exit area is too big relative to the size of the afterburner, or primary, nozzle. [19] This occurred under certain conditions on the J85 installation in the T-38. The secondary or final nozzle was a fixed geometry sized for the maximum afterburner case.

  6. Altitude compensating nozzle - Wikipedia

    en.wikipedia.org/wiki/Altitude_compensating_nozzle

    Altitude compensating nozzles address this loss of efficiency by changing the shape or volume of the rocket nozzle as the rocket climbs through the atmosphere. There are a wide variety of designs that achieve this goal, with the aerospike being perhaps the most studied among them. Aerospike engine; Plug nozzle; Expanding nozzle

  7. Aerospike engine - Wikipedia

    en.wikipedia.org/wiki/Aerospike_engine

    It uses carbon composite materials and uses the same basic design for both stages. The plug-cluster aerospike engine puts out 90,000 pounds-force (400 kN) of thrust. The engine has a bell-shaped nozzle that has been cut in half, then stretched to form a ring with the half-nozzle now forming the profile of a plug. [8]

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  9. 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 ...

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