Answer:
Part a)
[tex]a = 2.46 \times 10^4 g[/tex]
Part b)
[tex]a = 100.37 g[/tex]
Explanation:
Part a)
During the launch
speed will increase from rest to final speed of 1.60 m/s
the distance moved by it is given as
[tex]d = 5.30 \mu m[/tex]
now we have
[tex]v_f^2 - v_i^2 = 2ad[/tex]
[tex]1.60^2 - 0 = 2(a)(5.30 \times 10^{-6})[/tex]
so we have
[tex]a = \frac{1.60^2}{2(5.30 \times 10^{-6})}[/tex]
[tex]a = 2.4151 \times 10^5 m/s^2[/tex]
now in terms of g it is given as
[tex]a = 2.46 \times 10^4 g[/tex]
Part b)
During speed reduction
we know that final speed will be zero by air in distance 1.30 mm
so we have
[tex]v_f^2 - v_i^2 = 2 a d[/tex]
[tex]0 - 1.60^2 = 2(a)(1.30 \times 10^{-3})/tex]
[tex]a = 984.6 m/s^2[/tex]
Now in terms of g it is
[tex]a = 100.37 g[/tex]