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One of the design requirements for a multirole jet fighter requires certain performance at 5000 m MSL (Mean Sea Level) in a Tropical climate (i.e. the US Standard Atmosphere is not the relevant model). What atmospheric conditions (P, T, and ?) would you use in calculations that determine if a proposed design can meet this requirement? Assume the Tropical Atmosphere parameter values at sea level are the following: T0 = 302.4 K, P0 = 101,325 Pa, ?0 = 1.167 kg/m3. The lapse rate Th is -6.0 K/km indicating a cooling in the atmosphere with height. Assume that the jet fighter operates in the Troposphere (i.e. the lapse rate is constant).

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