| getThrustVector(AbsoluteDate) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getIsp(AbsoluteDate) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getFlowRate(AbsoluteDate) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getDirection(AbsoluteDate) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getThrustMagnitude(AbsoluteDate) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, Control3DVectorCostType, String) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| ConstantThrustManeuver(AbsoluteDate, double, AttitudeProvider, AbstractConstantThrustPropulsionModel) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D, String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| ConstantThrustManeuver(AbsoluteDate, double, double, double, AttitudeProvider, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isFiring(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| ConstantThrustManeuver(AttitudeProvider, DateBasedManeuverTriggers, AbstractConstantThrustPropulsionModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| isFiring(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustVector() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIsp() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFlowRate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDirection() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStartDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEndDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDuration() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| isFiring(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustMagnitude() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |