PropulsionModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total2 of 2190%0 of 0n/a151615
getName()20%n/a111111
init(FieldSpacecraftState, FieldAbsoluteDate)7100%n/a010201
getFieldEventDetectors(Field)6100%n/a010101
getEventDetectors()5100%n/a010101
init(SpacecraftState, AbsoluteDate)1100%n/a010101