| ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D, String) |   | 93% | | 100% | 0 | 2 | 2 | 19 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 91% | | 50% | 1 | 2 | 1 | 5 | 0 | 1 |
| lambda$getFieldEventsDetectors$3(FieldSpacecraftState, FieldDateDetector, boolean) | | 80% | | 50% | 1 | 2 | 0 | 2 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) | | 100% | | 100% | 0 | 11 | 0 | 8 | 0 | 1 |
| getFieldEventsDetectors(Field) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| getEventsDetectors() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| acceleration(FieldSpacecraftState, RealFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| addContribution(FieldSpacecraftState, FieldTimeDerivativesEquations) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| addContribution(SpacecraftState, TimeDerivativesEquations) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getISP() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$getEventsDetectors$1(SpacecraftState, DateDetector, boolean) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| ConstantThrustManeuver(AbsoluteDate, double, double, double, Vector3D) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| lambda$getFieldEventsDetectors$2(FieldSpacecraftState, FieldDateDetector, boolean) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| lambda$getEventsDetectors$0(SpacecraftState, DateDetector, boolean) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getThrust() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFlowRate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| dependsOnPositionOnly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |