PropulsionModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total2 of 1283%0 of 0n/a141514
getName()20%n/a111111
init(FieldSpacecraftState, FieldAbsoluteDate)7100%n/a010201
getParametersDrivers()2100%n/a010101
init(SpacecraftState, AbsoluteDate)1100%n/a010101