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IAgVAState Interface

Description

Spacecraft Parameters properties for the spacecraft configuration.

Public Methods

Public Method GetInFrameNameGets the orbit state in the specified frame.
Public Method SetElementTypeSets the element type.

Public Properties

Public Property CdThe dimensionless drag coefficient associated with the drag area. Dimensionless.
Public Property CoordSystemNameThe coordinate system.
Public Property CrThe reflectivity of the spacecraft used for solar radiation pressure calculations, where 2.0 is fully reflective and 1.0 is not reflective at all. Dimensionless.
Public Property DragAreaThe cross-sectional area of the spacecraft assumed perpendicular to the direction of motion, used for atmospheric drag calculations. Uses SmallArea Dimension.
Public Property DryMassThe mass of the spacecraft exclusive of propellant. Uses Mass Dimension.
Public Property ElementReturns the currently selected element type.
Public Property ElementTypeThe element type.
Public Property EpochThe epoch of the Orbit State. Uses DateFormat Dimension.
Public Property FuelDensityThe density of the fuel tank. Uses SmallDensity Dimension.
Public Property FuelMassThe mass of the spacecraft propellant. Uses Mass Dimension.
Public Property K1If you are using a non-spherical SRP model, this field defines the model's GPS solar radiation pressure K1 (scale) value. Dimensionless.
Public Property K2If you are using a non-spherical SRP model, this field defines the model's GPS solar radiation pressure K2 (scale) value. Dimensionless.
Public Property RadiationPressureAreaThe cross-sectional area of the spacecraft assumed perpendicular to the direction of central body radiation, used for central body radiation (albedo / thermal pressure) calculations. Uses Small Area Dimension.
Public Property RadiationPressureCoeffThe reflectivity of the spacecraft used for central body radiation pressure (albedo / thermal pressure) calculations, where 2.0 is fully reflective and 1.0 is not reflective at all. Dimensionless.
Public Property SRPAreaThe cross-sectional area of the spacecraft assumed perpendicular to the direction of solar radiation, used for solar radiation calculations. Uses SmallArea Dimension.
Public Property TankPressureThe fuel tank pressure. Uses Pressure Dimension.
Public Property TankTemperatureThe temperature of the fuel tank. Uses Temperature Dimension.

Interfaces

Implemented Interface

CoClasses that Implement IAgVAState

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