Path: SC/SystemDesign
% Mass breakdown of JHU APL satellites. Provides a subsystem mass breakdown for four representative satellites. The last column is the fraction of the total mass, for rows that are subsystem masses. -------------------------------------------------------------------------- Form: JHAPLSatelliteMass; % demo m = JHAPLSatelliteMass( s, 'all' ) % table m = JHAPLSatelliteMass( s, p ) % subsystem mass -------------------------------------------------------------------------- ------ Inputs ------ s '' Satellite, 'messenger' 'stereo a' 'stereo b' 'new horizons' p (1,1) Parameter, 'all' or a named parameter from the list: 'total power' 'vol' 'mass' 'payload' 'structure' 'propulsion' 'fuel' 'power' 'comm' 'cdh' 'acs' 'thermal' 'harness' ------- Outputs ------- m {:,3} [name value fraction (if mass)] - or - m (1,1) if not 'all' for p -------------------------------------------------------------------------- References: Schaefer, E.D., et. al.,"Spacecraft Packaging", Johns Hopkins APL Technical Digest, Vol. 28, No. 1 2008. --------------------------------------------------------------------------
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