Data Providers: Aircraft: Astrogator Values: Maneuver

Aircraft: Astrogator Values: Maneuver

Maneuver related Calc Objects.

Name	Dimension	Type	Description
Time	DateFormat	Real Number	Time.
DeltaV	Rate	Real Number	Delta-V magnitude integrated along the trajectory path.
FuelMass	MassUnit	Real Number	Fuel mass remaining.
Fuel_Density	SmallDensity	Real Number	Density of the fuel.
Fuel_Used	MassUnit	Real Number	Fuel used since the initial state of the spacecraft.
Inertial_DeltaV_Magnitude	Rate	Real Number	The magnitude of accumulated Delta-V integrated in inertial coordinates. Computed by integrating the thrust acceleration over time.
Inertial_DeltaVx	Rate	Real Number	The X component of accumulated Delta-V integrated in inertial coordinates.
Inertial_DeltaVy	Rate	Real Number	The Y component of accumulated Delta-V integrated in inertial coordinates.
Inertial_DeltaVz	Rate	Real Number	The Z component of accumulated Delta-V integrated in inertial coordinates.
Specific_Impulse	SpecificImpulseUnit	Real Number	The specific impulse during the maneuver, accounting for all engines, computed using the rocket equation.
Tank_Pressure	PressureUnit	Real Number	Fuel tank pressure.
Tank_Temperature	Temperature	Real Number	Fuel tank temperature.
Thrust_Vector_X	ForceUnit	Real Number	The X component of the total thrust vector. The Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
Thrust_Vector_Y	ForceUnit	Real Number	The Y component of the total thrust vector. The Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
Thrust_Vector_Z	ForceUnit	Real Number	The Z component of the total thrust vector. The Calc Object allows a choice of coordinate systems. The default is Earth Centered Inertial.
Total_Mass	MassUnit	Real Number	Total mass (fuel plus dry mass).
Total_Mass_Flow_Rate	Mass Per Time	Real Number	The total mass flow rate, accounting for all engines, during a maneuver.