A rocket motor is manufactured by bonding together two types of propellants, an igniter and a sustainer. The shear strength of the bond ( y ) is thought to be a linear function of the age of the...


A rocket motor is manufactured by bonding together two types of propellants, an igniter and a sustainer. The shear strength of the bond (y) is thought to be a linear function of the age of the propellant (x) when the motor is cast. Twenty observations are shown in the following table.















































































































Observation numberStrengthy (psi)Agex (weeks)
12158.715.5
21678.1523.75
323168
42061.317
52207.55
61708.319
71784.724
825752.5
92357.97.5
102277.711
112165.213
122399.553.75
131779.825
142336.759.75
151765.322
162053.518
172414.46
182200.512.5
192654.22
201753.721.5


Round your answers to 2 decimal places.<br>Find a 90.0% confidence interval on each of the following:<br>(a) Po-<br>-15.27<br>-15.27<br>(b) B1-<br>1.30<br>130<br>(c) Mean shear strength when agex- 14.25 weeks.<br>I i 3.19<br>i| 3.19<br>(d) Find a 90.0% prediction interval on shear strength when age x- 14.25 weeks.<br>3.19<br>3.19<br>

Extracted text: Round your answers to 2 decimal places. Find a 90.0% confidence interval on each of the following: (a) Po- -15.27 -15.27 (b) B1- 1.30 130 (c) Mean shear strength when agex- 14.25 weeks. I i 3.19 i| 3.19 (d) Find a 90.0% prediction interval on shear strength when age x- 14.25 weeks. 3.19 3.19

Jun 08, 2022
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