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
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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'
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Outputs
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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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