| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 6 of 162 | 96% | 0 of 0 | n/a | 2 | 12 | 2 | 22 | 2 | 12 |
| getThrustVector(AbsoluteDate) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| getFlowRate(AbsoluteDate) | | 0% | n/a | 1 | 1 | 1 | 1 | 1 | 1 | |
| ScaledConstantThrustPropulsionModel(double, double, Vector3D, String) | | 100% | n/a | 0 | 1 | 0 | 5 | 0 | 1 | |
| getThrustVector(CalculusFieldElement[]) | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| getParametersDrivers() | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getThrustVector(double, double, double) | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| getThrustVector() | | 100% | n/a | 0 | 1 | 0 | 3 | 0 | 1 | |
| getThrustVector(double[]) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getFlowRate(CalculusFieldElement[]) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| static {...} | | 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 |