VehiclePhysicalData =================== .. py:class:: ansys.stk.core.stkobjects.VehiclePhysicalData Class defining physical data for the LOP force model. .. py:currentmodule:: VehiclePhysicalData Overview -------- .. tab-set:: .. tab-item:: Properties .. list-table:: :header-rows: 0 :widths: auto * - :py:attr:`~ansys.stk.core.stkobjects.VehiclePhysicalData.drag_cross_sectional_area` - Get or set the satellite's cross-sectional area to be used in atmospheric drag calculations. Uses Area Dimension. * - :py:attr:`~ansys.stk.core.stkobjects.VehiclePhysicalData.solar_radiation_pressure_cross_sectional_area` - Get or set the satellite's cross-sectional area to be used in solar radiation pressure calculations. Uses Area Dimension. * - :py:attr:`~ansys.stk.core.stkobjects.VehiclePhysicalData.satellite_mass` - Get or set the mass of the satellite to be used in atmospheric drag and solar radiation pressure calculations. Uses Mass Dimension. Import detail ------------- .. code-block:: python from ansys.stk.core.stkobjects import VehiclePhysicalData Property detail --------------- .. py:property:: drag_cross_sectional_area :canonical: ansys.stk.core.stkobjects.VehiclePhysicalData.drag_cross_sectional_area :type: float Get or set the satellite's cross-sectional area to be used in atmospheric drag calculations. Uses Area Dimension. .. py:property:: solar_radiation_pressure_cross_sectional_area :canonical: ansys.stk.core.stkobjects.VehiclePhysicalData.solar_radiation_pressure_cross_sectional_area :type: float Get or set the satellite's cross-sectional area to be used in solar radiation pressure calculations. Uses Area Dimension. .. py:property:: satellite_mass :canonical: ansys.stk.core.stkobjects.VehiclePhysicalData.satellite_mass :type: float Get or set the mass of the satellite to be used in atmospheric drag and solar radiation pressure calculations. Uses Mass Dimension.