Ballast table for UF1 (not used because first race)
5% -> 30 kg
4% -> 24 kg
3% -> 18 kg
2% -> 12 kg
1% -> 6 kg
Ballast table for LX4
5% -> 24 kg
4% -> 19 kg
3% -> 14 kg
2% -> 9 kg
1% -> 4 kg
Ballast table for RAC
10% -> 80kg
9% -> 72kg
8% -> 64kg
7% -> 56kg
6% -> 48kg
5% -> 40kg
4% -> 32kg
3% -> 24kg
2% -> 16kg
1% -> 8kg
Ballast table for LX6
15% -> 80kg
14% -> 75kg
13% -> 70kg
12% -> 64kg
11% -> 59kg
10% -> 53kg
9% -> 48kg
8% -> 43kg
7% -> 37kg
6% -> 32kg
5% -> 26kg
4% -> 21kg
3% -> 16kg
2% -> 10kg
1% -> 5kg






	function calculateBallast (carMass, carPower, percent)
	 powerWeightRatio = carMass/carPower
	 newPowerWeightRatio = powerWeightRatio * (1+(percent/100))
	 newCarMass = newPowerWeightRatio * carPower
	 ballast = newCarMass - carMass
	 return math.floor(ballast)
	end

io.write ("Ballast table for UF1 (not used because first race)\n")
for i=5,1,-1 do
  io.write(i,"% -> ", calculateBallast (600 ,55, i),     " kg\n")
end


io.write ("Ballast table for LX4 \n")
for i=5,1,-1 do
  io.write(i,"% -> ", calculateBallast (499 ,140, i),     " kg\n")
end

io.write ("Ballast table for RAC \n")
for i=10,1,-1 do
  io.write(i,"% -> ",calculateBallast (800 ,245 , i),     "kg\n")
end

io.write ("Ballast table for LX6 \n")
for i=15,1,-1 do
  io.write(i,"% -> ",calculateBallast (539 ,190 , i),     "kg\n")
end