From the results of numerous measurements it is known that in the altitude range from H1 = 120 km to H2 = 160 km, the temperature in the atmosphere changes according to a linear law from T1 = 332 K to T2 = 1155 K. Determine the pressure P2 at altitude H2, if at altitude H1 it equals P1 = 2.5•10-3 Pa. The molar mass of air at such altitudes is m = 27.5 g/mol.

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