úΕ¹     Safe mult. ft. to get meters (exact)mult deg K to get deg Rmult lb/sq.ft to get sq.m mult slugscu.ft to get kgcu.msea-level temperature, kelvinssea-level pressure, N/sq.msea-level density, kg/cu.mspeed of sound at S.L. m/secviscosity constantSutherland'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     $       $atmos-0.4.0.0-BXfiD5pCaoC68N8pFmji5M AtmosphereAtmosphere.DimensionalAtmosphere.ConstantsAtmosatmosTemperature atmosPressure atmosDensityatmosSpeedOfSoundatmosViscosityatmosKinematicViscosity siAtmosphere usAtmospheresiAltitudeFromPressure atmospherealtitudeFromPressure _FT2METERS_KELVIN2RANKINE_PSF2NSM_SCF2KCM_TZERO_PZERO_RHOZERO_AZERO _BETAVISC_SUTH_REARTH_GMR htpgTablemetricViscosity