Two satellites A and B rotate round a planet’s orbit having radius 4R and R respectively. If the speed of satellite A is 3 V then speed of satellite B is
\(\frac {3V}{2}\)
6V
\(\frac {4V}{2}\)
12 V
The speed of an object in a circular orbit is given by the formula:
v = \(\sqrt{\frac {GM}{R}}\)
Let's compare the speeds of satellites A and B: For satellite A:
vA = \(\sqrt{\frac {GM}{4R}}\)
For satellite B:
vB = \(\sqrt{\frac {GM}{R}}\)
vA = \(\sqrt{\frac {GM}{4R}}\)
vA = \(\sqrt{\frac {1}{4}}\) \(\sqrt{\frac {GM}{R}}\)
vA = \(\frac {1}{2}\)vB
Therefore, the speed of satellite B is twice the speed of satellite A, which means:
vB = 2 vA
vB = 2 x 3V
vB = 6V
So, the correct option is (B) 6V.
Net gravitational force at the center of a square is found to be \( F_1 \) when four particles having masses \( M, 2M, 3M \) and \( 4M \) are placed at the four corners of the square as shown in figure, and it is \( F_2 \) when the positions of \( 3M \) and \( 4M \) are interchanged. The ratio \( \dfrac{F_1}{F_2} = \dfrac{\alpha}{\sqrt{5}} \). The value of \( \alpha \) is 

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