Answer :
Orbital period can be calculated as:
T1 = (2πr1)/v1
Where r1is the radius of the orbit and is given as follows:
Where ε0 is the absolute permittivity of free space and is given as = 8.854 × 10-12 N-1C2m-2
h is Planck’s constant and is given as 6.64 × 10-34 Js
e is charge on an electron and is equals to 1.6 × 10-19C
m is the mass of an electron, and is equals to 9.1 × 10-31 Kg
substituting the values, we get
⇒
On calculating, we get
T1 = 15.27 × 10-16 seconds
For n = 2, we get
⇒
On calculating, we get
T2 = 1.22 × 10-15 seconds
For n = 3, we get
⇒
On calculating, we get
T3 = 4.12 × 10-15 seconds.
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