SpacecraftParameters

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 66100%0 of 0n/a012025012
validate(double)7100%n/a010201
setSolarRadArea(double)7100%n/a010301
setSolarRadCoeff(double)7100%n/a010301
setDragArea(double)7100%n/a010301
setDragCoeff(double)7100%n/a010301
SpacecraftParameters()6100%n/a010301
setMass(double)6100%n/a010301
getSolarRadArea()4100%n/a010101
getSolarRadCoeff()4100%n/a010101
getDragArea()4100%n/a010101
getDragCoeff()4100%n/a010101
getMass()3100%n/a010101