JHAPLSatelliteMass:

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.
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   Form:
       JHAPLSatelliteMass;   % demo
   m = JHAPLSatelliteMass( s, 'all' )  % table
   m = JHAPLSatelliteMass( s, p )      % subsystem mass
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   ------
   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

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   References:	Schaefer, E.D., et. al.,"Spacecraft Packaging", Johns
               Hopkins APL Technical Digest, Vol. 28, No. 1 2008.
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