| getThrustVector(AbsoluteDate) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| getFlowRate(AbsoluteDate) | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| BasicConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustVector(CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| static {...} | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| BasicConstantThrustPropulsionModel(double, double, Vector3D, String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getThrustVector() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustVector(double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFlowRate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFlowRate(double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFlowRate(CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |