StructuralMass:
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Determine the mass available for airship structure and systems.
The lifting gas is assumed to be Helium.
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Form:
[m0,mT,mH] = StructuralMass( VMax, kSV, rhoF, alt, mP );
Example:
[m0,mT,mH] = StructuralMass( 736310.778, 0.065, 0.5, 21300, 1814 );
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Inputs
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VMax (1) Maximum volume [m^3]
kSV (1) Surface area -to- volume ratio
rhoF (1) Exterior fabric density [kg/m^2]
alt (1) Pressure altitude [m]
mP (1) Payload mass [kg]
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Outputs
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m0 (1) Mass available for structure and systems [kg]
mT (1) Total vehicle mass, including payload [kg]
mH (1) Mass of Helium [kg]
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Children:
Common: Atmosphere/StdAtm
Common: Graphics/NewFig
