1
MHT CET 2023 11th May Evening Shift
MCQ (Single Correct Answer)
+1
-0

The radius of the orbit of a geostationary satellite is (mean radius of earth is '$$R$$', angular velocity about own axis is '$$\omega$$' and acceleration due to gravity on earth's surface is '$$g$$')

A
$$\left(\frac{\mathrm{gR}^2}{\omega^2}\right)^{\frac{1}{3}}$$
B
$$\left(\frac{\mathrm{gR}^2}{\omega^2}\right)^{\frac{2}{3}}$$
C
$$\left(\frac{\mathrm{gR}^2}{\omega^2}\right)^{\frac{1}{2}}$$
D
$$\frac{\mathrm{gR}^2}{\omega^2}$$
2
MHT CET 2023 11th May Evening Shift
MCQ (Single Correct Answer)
+1
-0

The ratio of energy required to raise a satellite to a height '$$h$$' above the earth's surface to that required to put it into the orbit at the same height is ($$\mathrm{R}=$$ radius of earth)

A
$$\frac{2 \mathrm{~h}}{\mathrm{R}}$$
B
$$\frac{h}{R}$$
C
$$\frac{\mathrm{R}}{\mathrm{h}}$$
D
$$\frac{\mathrm{R}}{2 \mathrm{~h}}$$
3
MHT CET 2023 11th May Morning Shift
MCQ (Single Correct Answer)
+1
-0

The radius of earth is $$6400 \mathrm{~km}$$ and acceleration due to gravity $$\mathrm{g}=10 \mathrm{~ms}^{-2}$$. For the weight of body of mass $$5 \mathrm{~kg}$$ to be zero on equator, rotational velocity of the earth must be (in $$\mathrm{rad} / \mathrm{s}$$ )

A
$$\frac{1}{80}$$
B
$$\frac{1}{400}$$
C
$$\frac{1}{800}$$
D
$$\frac{1}{1600}$$
4
MHT CET 2023 11th May Morning Shift
MCQ (Single Correct Answer)
+1
-0

A body of mass '$$\mathrm{m}$$' kg starts falling from a distance 3R above earth's surface. When it reaches a distance '$$R$$' above the surface of the earth of radius '$$R$$' and Mass '$$M$$', then its kinetic energy is

A
$$\frac{2}{3} \frac{\mathrm{GMm}}{\mathrm{R}}$$
B
$$\frac{1}{3} \frac{\mathrm{GMm}}{\mathrm{R}}$$
C
$$\frac{1}{2} \frac{\mathrm{GMm}}{\mathrm{R}}$$
D
$$\frac{1}{4} \frac{\mathrm{GMm}}{\mathrm{R}}$$
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