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Answer
Time period T = 1.50 s
time t = 40 s
r = 6.2 m
a)
Angular speed ω = 2π/T
               = [tex]\dfrac{2\pi }{1.5}[/tex] Â
               = 4.189 rad/s
Angular acceleration α = [tex]\dfrac{\omega}{t}[/tex]
                   = [tex]\dfrac{4.189}{40}[/tex]
                   = 0.105 rad/s²
Tangential acceleration a = r α = 6.2 x 0.105 = 0.651 m/s²
b)The maximum speed.
    v = 2πr/T
     = [tex]\dfrac{2\pi \times 6.2}{1.5}[/tex]
     = 25.97 m/s
So centripetal acceleration.
    a = [tex]\dfrac{v^2}{r}[/tex]
     = [tex]\dfrac{25.97^2}{6.2}[/tex]
     =  108.781 m/s^2
     = 11.1 g  Â
in combination with the gravitation acceleration.
[tex]a_{total} = \sqrt{(11.1g)^2+g^2}[/tex]
[tex]a_{total}= 11.145 g[/tex]
a. The astronaut's tangential acceleration during the first 40.0 seconds is [tex]0.651 \;m/s^2[/tex]
b. The number of g's of acceleration the astronaut would experience when the device is rotating at top speed is 11.10g.
Given the following data:
- Time, t = 40 seconds
- Radius, r = 6.20 meter
- Period, T = 1.50 seconds
- Acceleration, a = 9.80 [tex]m/s^2[/tex] = 1 g.
- Initial angular velocity = 0 rad/s (since the centrifuge starts from rest).
a. To find the astronaut's tangential acceleration during the first 40.0 seconds:
First of all, we would determine the final angular speed of the astronaut.
[tex]w_f = \frac{2\pi}{T}\\\\w_f = \frac{2\times 3.142}{1.50}\\\\w_f = \frac{6.284}{1.50}[/tex]
Final angular speed = 4.189 rad/s
Next, we would determine the astronaut's angular acceleration:
[tex]w_f = w_o + at[/tex]
Where:
- [tex]w_f[/tex] is the final angular velocity.
- [tex]w_o[/tex] is the initial angular velocity.
- [tex]\alpha[/tex] is the angular acceleration.
- t is the time.
Substituting the parameters into the formula, we have;
[tex]4.189 = 0 + \alpha 40\\\\4.189 = \alpha 40\\\\\alpha =\frac{4.189}{40} \\\\\alpha = 0.105 rad/s^2[/tex]
Now, we can calculate the astronaut's tangential acceleration:
[tex]\alpha_t = \alpha r\\\\\alpha_t = 0.105\times 6.20\\\\\alpha_t = 0.651 m/s^2[/tex]
b. To find how many g's of acceleration the astronaut would experience when the device is rotating at top speed:
At top speed, the centripetal acceleration of the astronaut is given by:
[tex]\alpha_c = w^2r\\\\\alpha_c = 4.189^2\times 6.20\\\\\alpha_c = 17.55\times 6.20\\\\\alpha_c = 108.81 \;m/s^2[/tex]
In terms of g:
[tex]\alpha_c = \frac{108.81}{9.80} \\\\\alpha_c = 11.10g[/tex]
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