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Mere Teacher · Previous Year Questions
JEE Main Physics · Gravitation · Set 11 (Q301-330)
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301.
A planet revolves round the Sun in an elliptical orbit. The linear speed of the planet will be maximum at
(1)D
(2)B
(3)A
(4)C
302.
The dependence of acceleration due to gravity g on the distance r from the centre of the earth, assumed to be a sphere of radius R of uniform density is as shown in figures below. The correct figure is.
(1)
(2)
(3)
(4)
303.
The weight of a body on the surface of the earth is 100 N. The gravitational force on it when taken at a height, from the surface of earth, equal to one-fourth the radius of the earth is:
(1)64 N
(2)25 N
(3)50N
(4)100 N
304.
The percentage decrease in the weight of a rocket, when taken to a height of 32 km above the surface of earth will, be: (Radius of earth = 6400km)
(1)1%
(2)3%
(3)4%
(4)0.5%
305.
Infinite number of spheres, each of mass m are placed on the X-axis at distances 1,2,4,8,16, meters from origin. The magnitude of the gravitational field at the origin is
(1)32Gm
(2)34Gm
(3)Gm
(4)6Gm
306.
Two planets have masses M and 16M and their radii are a and 2a, respectively. The separation between the centres of the planets is 10 a. A body of mass m is fired from the surface of the larger planet towards the smaller planet along the line joining their centres. For the body to be able to reach the surface of smaller planet, the minimum firing speed needed is
(1)23a5GM
(2)maGM2
(3)2aGM
(4)4aGM
307.
Two particles of equal mass go around a circle of radius R under the action of their mutual gravitational attraction. The speed v of each particle is
(1)21RGm
(2)R4Gm
(3)2R1Gm1
(4).
308.
At some location on earth the horizontal component of earth's magnetic field is 18×10−6T. At this location, magnetic needle of length 0.12mand pole strength 1.8Am is suspended from its mid-point using a thread, it makes 45∘ angle with horizontal in equilibrium. To keepthis needle horizontal, the vertical force that should beapplied at one of its ends is:
(1)3.6×10−5N
(2)1.8×10−5N
(3)1.3×10−5N
(4)6.5×10−5N
309.
A satellite is orbiting just above the surface of the earth with period T. If d is the density of the earth and G is the universal constant of gravitation, the quantity Gd3π represents
(1)T2
(2)T3
(3)T
(4)T
310.
At what height from the surface of earth the gravitational potential and the value of g are −5.4×107 J kg−1 and 6.0 ms−2 respectively? Take the radius of earth as 6400 km
(1)2000 km
(2)2600 km
(3)1600 km
(4)1400 km
311.
Given below are two statements: one is labelled as Assertion (a)and the other is labelled as Reason (R). Assertion (A): The radius vector from the Sun to a planet sweeps out equal areas in equal intervals of time and thus areal velocity of planet is constant. Reason (R): For a central force field the angular momentum is a constant. In the light of the above statements, choose the most appropriate answer from the options given below:
(1)(A) is not correct but (R) is correct
(2)Both (A) and (R) are correct but (R) is not the correct explanation of (A)
(3)Both (A) and (R) are correct and (R) is the correct explanation of (A)
(4)(A) is correct but (R) is not correct
312.
At what height from the surface of earth the gravitational potential and the value of g are −5.4×107Jkg−1 and 6.0ms−2 respectively? Take, the radius of earth as 6400 km. [NEET 2016]
(1)1600 km
(2)1400 km
(3)2000 km
(4)2600 km
313.
Kepler's third law states that square of period of revolution (T) of a planet around the sun, is proportional to third power of average distance r between sun and plane i.e. T2 = Kr3 here K is constant If the masses of sun and planet are M and m respectively then as per Newton's law of gravitation force of attraction between them is F = r2GMm, here G is gravitational constant The relation between G and K is described as:
(1)GMK = 4π2
(2)K = G
(3)K = G1
(4)GK = 4π2
314.
Acceleration due to gravity.
(1)increases with altitude
(2)decreases with altitude
(3)is independent of altitude
(4)first decrease and then increases with altitude
315.
A period of geostationary satellite is
(1)30h
(2)24h
(3)48h
(4)12h
316.
Given below are two statements: Statement I: A satellite is moving around earth in the orbit very close to the earth surface. The time period of revolution of satellite depends upon the density of earth. Statement II: The time period of revolution of the satellite is T=2πgRe (for satellite very close to the earth surface), where Re radius of earth and g acceleration due to gravity. In the light of the above statements, choose the correct answer from the options given below:
(1)Both Statement I and Statement II are true
(2)Statement I is false but Statement II is true
(3)Statement I is true but Statement II is false
(4)Both Statement I and Statement II are false
317.
Every planet revolves around the sun in an elliptical orbit: (A) The force acting on a planet is inversely proportional to square of distance from sun. (B) Force acting on planet is inversely proportional to product of the masses of the planet and the sun (C) The centripetal force acting on the planet is directed away from the sun. (D) The square of time period of revolution of planet around sun is directly proportional to cube of semi-major axis of elliptical orbit. Choose the correct answer from the options given below:
(1)A and D only
(2)C and D only
(3)B and C only
(4)A and C only
318.
Choose the correct statement.
(1)Acceleration due to gravity increases with increasing altitude.
(2)Acceleration due to gravity is independent of mass of earth.
(3)A geostationary satellite can have a time period less than 24h.
(4)Acceleration due to gravity decreases with increasing depth assuming earth to be a sphere of uniform density.
319.
Find the acceleration of our galaxy, due to the nearest comparably sized galaxy. The approximate masses of each galaxy is 8×1011 solar mass and they are separated by 2 million light-years. Each galaxy has a diameter of 100000 light year. (Assume, 1 light year ≈1016m, gravitational constant, G≈10−10(kg2Nm2) and mass of sun (=2.0×1030kg)
(1)4×10−13m/s2
(2)2×10−13m/s2
(3)5×10−15m/s2
(4)5×10−13m/s2
320.
A planet of mass M, has two natural satellites with masses m1 and m2. The radii of their circular orbits are R1 and R2 respectively. Ignore the gravitational force between the satellites. Define v1, L1, K1 and T1 to be, respectively, the orbital speed, angular momentum, kinetic energy and time period of revolution of satellite 1; and v2, L2, K2 and T2 to be the corresponding quantities of satellite 2. Given m1/m2 = 2 and R1/R2 = 1/4, match the ratios in List-I to the numbers in List-II. List-IP.v2v1Q.L2L1R.K2K1S.T2T1List-II1.812.13.24.8
(1)P → 4; Q → 2; R → 1; S → 3
(2)P → 3; Q → 2; R → 4; S → 1
(3)P → 2; Q → 3; R → 1; S → 4
(4)P → 2; Q → 3; R → 4; S → 1
321.
A rocket is launched normal to the surface of the Earth, away from the Sun, along the line joining the Sun and the Earth. The Sun is 3 × 105 times heavier than the Earth and is at a distance 2.5 × 104 times larger than the radius of the Earth. The escape velocity from Earth's gravitational field is ve = 11.2km s–1. The minimum initial velocity (vs) required for the rocket to be able to leave the Sun-Earth system is closest to: (Ignore the rotation and revolution of the Earth and the presence of any other planet)
(1)vs = 72 km s–1
(2)vs = 22 km s–1
(3)vs = 42 km s–1
(4)vs = 62 km s–1
322.
Two particles of equal mass 'm' move in a circle of radius 'r' under the action of their mutual gravitational attraction. The speed of each particle will be:
(1)2rGM
(2)r4GM
(3)rGM
(4)4rGM
323.
A body of weight W is projected vertically upwards from earth's surface to reach a height above the earth which is equal to nine times the radius of earth. The weight of the body at that height will be:
(1)91W
(2)100W
(3)9W
(4)3W
324.
The distance between Sun and Earth is R. The duration of year if the distance between Sun and Earth becomes 3R will be:
(1)3 years
(2)3 years
(3)9 years
(4)33 years
325.
The orbital period of a geostationary satellite is
(1)2h
(2)5h
(3)24h
(4)12h
326.
The escape velocity from earth is 11.2 km/s. If a body is to be projected in a direction making an angle 45o to the vertical, then the escape velocity is
(1)11.2×2km/s
(2)11.2 km/s
(3)11.2/2km/s
(4)11.22km/s
327.
The satellite of mass m is orbiting around the earth in a circular orbit with a velocity v. What will be its total energy?
(1)3/4mv2
(2)1/2mv2
(3)mv2
(4)-1/2mv2
328.
Let ' gh ' and ' gd ' be the accelerations due to gravity at height ' h ' above the earth's surface and at depth ' d ' below the earth's surface respectively. If gh=gd then the relation between ' h ' and ' d ' is
(1)d=h
(2)d=2h
(3)d=4h
(4)d=2h
329.
If the earth suddenly shrinks to 641th of its original volume with its mass remaining the same, the period of rotation of earth becomes x24h. The value of x is
330.
If the acceleration due to gravity experienced by a point mass at a height h above the surface of earth is same as that of the acceleration due to gravity at a depth ah (h<<Re) from the earth surface. The value of αwill be_________.(use Re =6400 km)