| OrbitManeuver() |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| getAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setAcceleration(int, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getDv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setDv(int, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getThrust() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setThrust(int, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getDeployDv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| setDeployDv(int, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDate(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDuration(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDeltaMass(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setAccelerationInterpolation(OnOff) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setAccelerationMagnitudeSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setAccelerationDirectionSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDvMagSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDvDirSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setThrustEfficiency(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setThrustInterpolation(OnOff) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setThrustIsp(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setThrustMagnitudeSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setThrustDirectionSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDeployId(String) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDeployMass(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDeployDvSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDeployDirSigma(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDeployDvRatio(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setDeployDvCda(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDuration() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeltaMass() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAccelerationInterpolation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAccelerationMagnitudeSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAccelerationDirectionSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDvMagSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDvDirSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustEfficiency() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustInterpolation() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustIsp() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustMagnitudeSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getThrustDirectionSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeployId() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeployMass() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeployDvSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeployDirSigma() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeployDvRatio() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeployDvCda() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |