| getControl3DVectorCostType() |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getFieldEventDetectors(Field) |  | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
| getEventDetectors() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
| shortestSegmentDuration() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| getThrustVector(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getThrustVector(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| ProfileThrustPropulsionModel(TimeSpanMap, double, Control3DVectorCostType, String) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getFlowRate(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFlowRate(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustVector(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFlowRate(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getName() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |