Path: AerospaceUtils/AtmosphericCalculations
% Compute the atm. density (kg/m^3) on Neptune given the altitude (km)
This is a third degree polynomial fit.
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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: CommonData/SwooshWatermark Common: General/CellToMat Common: General/MatToCell Common: General/Watermark Common: Graphics/NewFig Common: Graphics/Plot2D Common: Graphics/PltStyle
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