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    In aviation, pressure altitude is the indicated altitude when an altimeter is set to 1013 hPa (29.92 inHg US and Canada). It is primarily used in aircraft performance calculations, and in high-altitude flight (Class A airspace in the United States, which is controlled airspace at or above 18,000 feet).
    The relation between static pressure and pressure altitude is defined in terms of the properties of the International Standard Atmosphere (ISA). Up to 36,090 ft this relation can be expressed as:


    z =left (1-left( rac
    ight)^
    ight ) imes rac


    Where:

      z = pressure altitude (feet)
      P_o = static pressure (hPa)


        Pressure altitude
            Simplification
            See also

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    Simplification
    One simplification of the Pressure Altitude that is a bit more practical to pilots than the above formula is the following:


    A_~=~A_~+~(~29.92~inHg-P_)
      1000~ft/inHg.


    Where
      A_ = Pressure Altitude (z of the previous equation),
      A_ = Physical Altitude above Sea Level,
      P_ = Measured or estimated Pressure at the Altitude of interest in inches of mercury (inHg).

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    See also




     
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    Scientus.org Dictionary (Yet Another Wiki) RC : 1.39
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    This article is licensed under the GNU Free Documentation License [copyleft]. It uses material from the Wikipedia article "Pressure altitude". link