| Element | Missed Instructions | Cov. | Missed Branches | Cov. | Missed | Cxty | Missed | Lines | Missed | Methods |
| Total | 16 of 111 | 85% | 0 of 6 | 100% | 1 | 10 | 2 | 24 | 1 | 7 |
| getIsp(SpacecraftState) | | 0% | n/a | 1 | 1 | 2 | 2 | 1 | 1 | |
| getAcceleration(FieldSpacecraftState, FieldAttitude, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getAcceleration(SpacecraftState, Attitude, double[]) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getDirection(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getMassDerivatives(SpacecraftState, double[]) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getMassDerivatives(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 | |
| getExhaustVelocity(double) | | 100% | n/a | 0 | 1 | 0 | 1 | 0 | 1 |