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SUPPORT SITE |
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Path: SCPro/ProEnvirons
% Compute the atm. density (kg/m^3) on Neptune given the altitude (km)
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Form:
rho = NeptuneDensity( h )
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Inputs
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h (1,:) Altitude (km)
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Outputs
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rho (1,:) Density (kg/m^3)
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Reference: ATMOSPHERIC MODELS FOR AEROENTRY AND AEROASSIST
C. G. Justus, Aleta Duvall, Vernon W. Keller
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Common: Graphics/Plot2D
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