Maneuver components are a subset of Calculation Object components.
ComponentBrowser */ SetValue "Calculation Objects" {Component} {Attribute} <Value> [{Unit}]
ComponentBrowser */ Duplicate "Calculation Objects" {Component} <Duplicate Component Name>
The Maneuver components are:
| Component | Description |
|---|---|
| DeltaV | DeltaV integrated along path |
| FuelMass | Total fuel mass |
| Fuel Density | Fuel Density |
| Fuel Used | Fuel mass used during a segment |
| Inertial DeltaV Magnitude | Magnitude of accumulated DeltaV integrated in inertial coordinates |
| Inertial DeltaVx | X component of accumulated DeltaV integrated in inertial coordinates |
| Inertial DeltaVy | Y component of accumulated DeltaV integrated in inertial coordinates |
| Inertial DeltaVz | Z component of accumulated DeltaV integrated in inertial coordinates |
| Specific Impulse | Specific impulse during a maneuver |
| Tank Pressure | Tank Pressure |
| Tank Temperature | Tank Temperature |
| Thrust Vector X | X component Total Thrust Vector in inertial axes |
| Thrust Vector Y | Y component Total Thrust Vector in inertial axes |
| Thrust Vector Z | Z component Total Thrust Vector in inertial axes |
| Total Mass | Total Mass |
| Total Mass Flow Rate | Total Mass Flow Rate during a maneuver |
The attributes for each component have the same names and value selections that appear in the Astrogator graphical user interface.
This Maneuver component is defined by the following equation:
This is the scalar 
V integrated along the path of a spacecraft. Thus, we
are using the scalar acceleration athrust,
where
This integration occurs simultaneously with the orbit integration during a maneuver.
ComponentBrowser */ Duplicate "Calculation Objects" DeltaV "My DeltaV"
ComponentBrowser */ SetValue "Calculation Objects" "My Inertial DeltaVx" CoordAxes "CentralBody/Earth Fixed"
STK Programming Interface 11.0.1