Name
|
Description
|
Attributes
|
DeclaredName
|
The name of the object as declared.
|
Type: String
Access: Read-Only
|
DisplayName
|
The name displayed for this object in output windows such as views, plots, and reports.
|
Type: String
Access: Read/Write
|
MOI
|
The tank moment of inertia tensor.
|
Type: Matrix
Access: Read-Only
Units: kg m^2
|
ObjectId
|
The unique identifier for the object.
|
Type: Variable
Access: Read-Only
|
ObjectType
|
The type of the object.
|
Type: String
Access: Read-Only
|
TankCenterOfGravity
|
The center of gravity associated with the fuel mass in the tank. This location is determined based on the tank's reference location, fill line orientation, tank volume, fuel mass, and fuel density. The location is referenced from the origin of the Spacecraft BCS and is measured in meters.
|
Type: Array
Access: Read-Only
Units: m
|
TankMass
|
The current mass of the mass source in the Tank. This property is updated as mass is consumed.
|
Type: Variable
Access: Read/Write
Units: kg
|
TankMassDensity
|
The density of the mass source in used in the calculation of the center of gravity and moments of inertia calculations.
|
Type: Variable
Access: Read/Write
Units: kg/m^3
|
TankOrientation
|
The unit vector in the Spacecraft body coordinate system that defines the primary axis (or z-axis) of the tank. The tank's fill line is oriented perpendicular to this axis. The tank's center of gravity is determined based on this fill line orientation, the tank reference location, tank volume, fuel mass, and fuel density.
|
Type: Array
Access: Read/Write
|
TankPower
|
The power level supplied by the Tank. The power is used in the calculation of Thrust based on the respective Thruster coefficients. This property functions equivalently to the pressure property of a chemical tank and thruster with the ratio of temperature to reference temperature set to 1.
|
Type: Variable
Access: Read/Write
Units: kW
|
TankReference
|
The geometric center of the tank. This location is referenced from the origin of the Spacecraft BCS. The tank's center of gravity is determined based on this reference location, the fill line orientation, tank volume, fuel mass, and fuel density.
|
Type: Array
Access: Read/Write
Units: m
|
