SpacecraftParameters

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 69100%0 of 0n/a012029012
SpacecraftParameters()18100%n/a010701
validate(double)6100%n/a010201
setMass(double)6100%n/a010301
setSolarRadArea(double)6100%n/a010301
setSolarRadCoeff(double)6100%n/a010301
setDragArea(double)6100%n/a010301
setDragCoeff(double)6100%n/a010301
getMass()3100%n/a010101
getSolarRadArea()3100%n/a010101
getSolarRadCoeff()3100%n/a010101
getDragArea()3100%n/a010101
getDragCoeff()3100%n/a010101