Declared in FuelTransferMessage
Declaration
[Unit("kg")]
[Range(0, 1.7976931348623157E+308)]
double SourceAmount;Description
Remaining propellant mass in the source tank [kg].
Declared in FuelTransferMessage
[Unit("kg")]
[Range(0, 1.7976931348623157E+308)]
double SourceAmount;Remaining propellant mass in the source tank [kg].