Computes temperature (temp), pressure (pres) and density (dens) at a given altitude (alt),
following US 76 atmosphere model.
NOTE: 1 US 76 atmosphere model is only envisaged for altitudes up to 10^6 m (1000km).
2 If input altitude is negative, computation is performed for alt = 0 m
Last update : 24/08/2007
Parameters
alt:
altitude [m] (1xN)
temp:
kinetic temperature [K] (1xN)
pres:
pressure [Pa] (1xN)
dens:
density [kg/m^3] (1xN)
Authors
CNES - DCT/SB
Bibliography
1 CNES - MSLIB FORTRAN 90, Volume P (mp_atm_US76)
Examples
alt = 700.e3;
[temp,pres,dens] = CL_mod_atmUS76(alt)
See 'CelestLab > Demos > GEOPHYSICS > US76_atmosphere_model' for examples