| AbstractConstantThrustPropulsionModel(double, double, Vector3D, String) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| getIsp() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getDirection() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrust() | | 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 |
| getThrustVector(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFlowRate(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInitialThrustVector() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInitialFlowrate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getName() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustVector(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFlowRate(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |