úÎm      Safe mult. ft. to get meters (exact)!mult deg K to get deg R"mult lb/sq.ft to get sq.m# mult slugscu.ft to get kgcu.m$sea-level temperature, kelvins%sea-level pressure, N/sq.m&sea-level density, kg/cu.m'speed of sound at S.L. m/sec(viscosity constant)Sutherland's constant, kelvins*radius of the Earth, km+ gas constant,Ltable of (height, temperature, pressure, temperature gradient) over altitude !"#$%&'()*+, !"#$%&'()*+, !"#$%&'()*+,Safeatmosphere in SI unitsInput: altitude in metersKOutput: (pressure, density, speed of sound, viscosity, kinematic viscosity) Œpressure - N/m^2 density - kg/m^3 speed of sound - m/s viscosity - N-s/m^2 kinematic viscosity - m^2/s atmosphere in imperial unitsInput: altitude in ftKOutput: (pressure, density, speed of sound, viscosity, kinematic viscosity) ™pressure - lb/ft^2 density - slugs/ft^3 speed of sound - ft/s viscosity - slugs/(ft-s) kinematic viscosity - ft^2/s ICompute altitude at which the standard atmosphere has a certain pressure.Input: Pressure, N/m^2Output: Altitude in meters BCompute temperature, density, and pressure in standard atmosphere./Correct to 86 km. Only approximate thereafter."Input: alt geometric altitude, km.Output: (sigma, delta, theta) †sigma - density/sea-level standard density delta - pressure/sea-level standard pressure theta - temperature/sea-level std. temperature  -    - None     None   .           atmos_9tfhJAIIzQm16nCY5jvsz3 AtmosphereAtmosphere.DimensionalAtmosphere.DimensionalTFAtmosphere.ConstantsAtmosatmosTemperature atmosPressure atmosDensityatmosSpeedOfSoundatmosViscosityatmosKinematicViscosity siAtmosphere usAtmospheresiAltitudeFromPressure atmospherealtitudeFromPressure _FT2METERS_KELVIN2RANKINE_PSF2NSM_SCF2KCM_TZERO_PZERO_RHOZERO_AZERO _BETAVISC_SUTH_REARTH_GMR htpgTablemetricViscosity