According to Kepler's Law, the time period does not depend upon the mass of the satellite it only depends upon the orbital radius.
1:2
1:16
1:32
1:2√2
The mass of a satellite does not affect the time period
\(\frac{T_{A}}{T_{B}}=\left(\frac{r_{1}}{r_{1}}\right)^{3 / 2}=\left(\frac{r}{2 r}\right)^{3 / 2}=\left(\frac{1}{8}\right)^{1 / 2}=\frac{1}{2 \sqrt{2}}\)
\(\therefore \) TA= TB = 1:2√2
Hence, the correct option is d) 1:2√2.
Correct option (d) \(1:2\sqrt2\)
Explanation: According to Kepler's Law, the time period does not depend upon the mass of the satellite it only depends upon the orbital radius.
As T2 ∝ r3
TA/T =
\[{r^{3/2} \over 2 ^{3/2} r^{3/2}}\]So, their time periods are in the ratio of 1:2√2.
The correct option is D)
The mass of the satellite does not affect the time period
\(\frac{T_A}{T_B} = (\frac{r_1}{r_2})\frac{3}{2}\)
= \((\frac{r}{2r})\frac{3}{2}\)
= \((\frac{1}{8})\frac{1}{2}\)
= \(\frac{1}{2}\sqrt{2}\)
∴ \(T_A =T_B\) = 1:2\(\sqrt{2}\)
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On combining equations (1) and (2) we get,
F ∝ M1M2/r2
F = G × [M1M2]/r2 . . . . (7)
Or, f(r) = GM1M2/r2
The dimension formula of G is [M-1L3T-2].