1
COMEDK 2024 Evening Shift
MCQ (Single Correct Answer)
+1
-0

The acceleration due to gravity at pole and equator can be related as

A
$$g_e=g_p < g$$
B
$$g_e=g_p=g$$
C
$$g_e < g_p$$
D
$$g_e > g_p$$
2
COMEDK 2024 Evening Shift
MCQ (Single Correct Answer)
+1
-0

A satellite is revolving around the earth in a circular orbit with kinetic energy of $$1.69 \times 10^{10} \mathrm{~J}$$. The additional kinetic energy required for just escaping into the outer space is

A
$$3.38 \times 10^{10} \mathrm{~J}$$
B
$$1.69 \times 10^{10} \mathrm{~J}$$
C
$$0.89 \times 10^{10} \mathrm{~J}$$
D
$$1.35 \times 10^{10} \mathrm{~J}$$
3
COMEDK 2024 Afternoon Shift
MCQ (Single Correct Answer)
+1
-0

A planet has double the mass of the earth and double the radius. The gravitational potential at the surface of the Earth is $$\mathrm{V}$$ and the magnitude of the gravitational field strength is $$\mathrm{g}$$. The gravitational potential and gravitational field strength on the surface of the planet are

Potential Field
A V $$\frac{g}{4}$$
B 2V $$\frac{g}{2}$$
C V $$\frac{g}{2}$$
D 2V $$\frac{g}{4}$$

A
C
B
D
C
A
D
B
4
COMEDK 2024 Afternoon Shift
MCQ (Single Correct Answer)
+1
-0

Energy required for moving a body of mass $$\mathrm{m}$$ from a circular orbit of radius 3R to a higher orbit of radius 4R around the earth is.

A
$$ \frac{\mathrm{GMm}}{\mathrm{R}} $$
B
$$ \frac{\mathrm{GMm}}{24 \mathrm{R}} $$
C
$$ \frac{\mathrm{GMm}}{4 \mathrm{R}} $$
D
$$ \frac{\mathrm{GMm}}{12 \mathrm{R}} $$
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