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SUPPORT SITE |
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SUPPORT SITE |
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Path: SC/Environs
% Computes the atmospheric density of Mars. For h > 100 km the temperature is kept constant. Type AtmDensMars2 for a demo. -------------------------------------------------------------------------- Form: [rho, t, p] = AtmDensMars2( h ) -------------------------------------------------------------------------- ------ Inputs ------ h (1,:) Altitude (km) ------- Outputs ------- rho (1,:) Atmospheric Density (kg/m^3) p (1,:) Pressure (N/m^2) t (1,:) Temperature (deg-K) -------------------------------------------------------------------------- Reference: http://www.grc.nasa.gov/WWW/K-12/airplane/atmosmrm.html --------------------------------------------------------------------------
Common: Graphics/Plot2D
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