Arocket motor is manufactured by bonding togethertwo types of propellants, an igniter and a sustainer. the shearstrength of the bond y is thought to be a linear function of theage of the propellant x when the motor is cast. table e11-4provides 20 observations. find a 95% prediction interval on shear strength when agex = 20 weeks.# | psi(y) | age(x)1 2158.70 15.502 1678.15 23.753 2316.00 8.004 2061.30 17.005 2207.50 5.006 1708.30 19.007 1784.70 24.008 2575.00 2.509 2357.90 7.5010 2277.70 11.0011 2165.20 13.0012 2399.55 3.7513 1779.80 25.0014 2336.75 9.7515 1765.30 22.0016 2053.50 18.0017 2414.40 6.0018 2200.50 12.5019 2654.20 2.0020 1753.70 21.50