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Gravitation Test - 29

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Gravitation Test - 29
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  • Question 1
    1 / -0
    The ratio of escape velocity of a tennis ball to that of a basket ball on the surface of the earth is
    Solution
    Equating KE and PE we get the expression for escape velocity as $$\sqrt{2GM/r}$$, where M = mass of earth , r = radius of earth and G = gravitational constant. ince escape velocity is independent of mass of ball,  the ratio of escape velocity of a tennis ball to that of a basket ball on the surface of the earth is 1:1.
  • Question 2
    1 / -0
    A satellite S is moving in an elliptical orbit around the earth. The mass of the satellite is very small compared to the mass of the earth
    Solution
    In case of orbital motion, only angular momentum is conserved, i.e. mvr is constant. Thus v,r changes accordingly. Therefore, linear momentum mv is not constant in elliptical orbit. So option D is wrong
    The total mechanical energy is given by $$ \dfrac{-GMm}{2r} $$ which is independent of time. So, option C is wrong
    Both, direction and magnitude of angular momentum does not change. i.e. $$ r \times mv$$ is constant. So, B is also wrong.
    The gravitational force always towards the centre of the earth and thus the acceleration is always directed to the centre of earth. So, A is right.
  • Question 3
    1 / -0
    The distance from the surface of the earth at which above and below the surface acceleration due to gravity is same will be
    Solution
    Let the distance be $$d$$.
    For the condition:
    $$g\left(1-\dfrac{ h }{ R }\right) =g\left(\dfrac { R }{ R+h } \right)^2 $$
    $$\left(1-\dfrac { h }{ R }\right) \left(1+\dfrac { h }{ R }\right)^{ 2 }=1$$
    Solving this we get:
    $$h=\dfrac { \sqrt { 5 } -1 }{ 2 } R$$

  • Question 4
    1 / -0
    A satellite in earth orbit experiences a small drag force as it enters the earth's atmosphere. Two students were asked consequence of this
    Student-A : The satellite would slow down as, it spirals towards earth due to work of frictional force.
    Student-B : The satellite speed up due to earths gravitational pull as it spirals towards earth.
    Solution
    Let, $$U + K = c$$ where c is some constant. As the body spirals down, $$ U \downarrow, K \uparrow$$. Thus, speed of the satellite increases and the influence of air friction is negligable.
  • Question 5
    1 / -0
    Satellites A and B are orbiting around the earth in orbits of ratio $$R$$ and $$4R$$ respectively. The ratio of their areal velocities is
    Solution
    Using Kepler's second law we have:
    $$Areal \;velocity =\dfrac{Area  swept}{time}=\dfrac{\dfrac{1}{2}r(rd\theta)}{dt}=\dfrac{1}{2}r^2\omega=\dfrac{1}{2}rv=constant$$

    Thus we get, $$\dfrac{1}{2}\sqrt{\dfrac{GM}{r}}r$$     (from $$\dfrac{mv^2}{r}=\dfrac{GMm}{r^2}$$)
    Thus we get
    Areal velocity $$\propto \sqrt{r}$$
    Thus for the planets with radius in ratio of $$1:4$$ we get radii in the ratio of $$1:2$$
  • Question 6
    1 / -0
    A planet of radius $$R = 1/10 \times $$ (radius of Earth) has the same mass density as Earth. Scientists dig a well of depth $$R/5$$ on it and lower a wire of the same length and of linear mass density $$10^{-3} kgm^{-3}$$ into it. If the wire is not touching anywhere, the force applied at the top of the wire by a person holding it in place is (take the radius of Earth $$= 6 \times 10^6 m$$ and the acceleration due to gravity on Earth is $$10 ms^{-2}$$)
    Solution
    $$R_e$$ is the radius of the earth
    $$g_e=\dfrac{GM_e}{R_e^2}=G\dfrac{4}{3}\pi R_e\rho$$
    Now g at the mentioned planet is given as
    $$g_p=\dfrac{GM}{r^2}$$, here $$m=\dfrac{4}{3}\pi r^3\rho$$
    Thus $$g_p=\dfrac{4}{3}r\rho$$
    Thus we get $$F=\displaystyle\int^R_{4R/5}\lambda g_p dr = 108  N$$
  • Question 7
    1 / -0
    Two planets  $$A$$  and $$B$$  have the same material density. If the radius of  $$A$$  is twice that of B, then the ratio of the escape velocity $$\displaystyle \dfrac{V_A}{V_B}$$ is
    Solution
    Let the density be d for both the planets. Given that $$R_A = 2R_B$$
    Now, mass of $$A,\ M_A = \dfrac{4d\pi {R_A}^3}{3} = \dfrac{32d\pi {R_B}^3}{3}$$
    similarly, $$M_B = \dfrac{4d\pi {R_B}^3}{3}$$
    Escape velocity for a planet is given by $$V =\sqrt{\dfrac{2GM}{R}}$$

    So, $$V_A = \sqrt{\dfrac{2GM_A}{3R_A}} = \sqrt{\dfrac{64Gd\pi {R_B}^3}{6R_B}} = \sqrt{\dfrac{32Gd\pi {R_B}^2}{3}}$$

    Similarly, $$V_B = \sqrt{\dfrac{8Gd\pi {R_B}^2}{3}}$$

    Taking the ratio, $$\dfrac{V_A}{V_B} = \sqrt{\dfrac{32Gd\pi {R_B}^2}{3}} \times \sqrt{\dfrac{3}{8Gd\pi {R_B}^2}} =2$$
  • Question 8
    1 / -0
    A planet revolves about the sun in elliptical orbit. The arial velocity $$\displaystyle \left ( \frac{dA}{dt} \right )$$ of the planet is $$4.0 \times 10^{16} m^2/s$$. The least distance between planet and the sun is $$2 \times 10^{12}$$m. Then the maximum speed of the planet in km/s is
    Solution
    We have: $$\dfrac{dA}{dt}=\dfrac{1}{2}r^2\dfrac{d\theta}{dt}$$

    $$4\times 10^{16}=\dfrac{1}{2}(2\times 10^{12})^2\dfrac{d\theta}{dt}$$

    $$\omega=\dfrac{d\theta}{dt}=2\times 10^{-8}$$

    Using, $$v=r\omega$$ 
    We get: $$v=2\times 10^{12}\times 2\times 10^{-8}=40\ km/s  $$
  • Question 9
    1 / -0
    A (nonrotating) star collapses onto itself from an initial radius R$$_i$$ with its mass remaining unchanged. Which curve in figure best gives the gravitational acceleration a$$_g$$ on the surface of the star as a function of the radius of the star during the collapse?

    Solution
    $$g\propto \dfrac{1}{R^2}$$
    Curve b represents this variation.
  • Question 10
    1 / -0
    Select the correct choice(s)
    Solution
    Gravitational field is conservative field, total mechanical energy is conserved.
    If a body is in gravitational field with $$ U + K = 0 \rightarrow  K = -U \rightarrow (1)$$ i.e. Kinetic energy is non zero.So, it will move away from the field till its kinetic energy is also zero.
    If $$K = 0 \rightarrow$$ U = 0 from (1). But, U = 0 is at $$\infty$$ and thus the body escapes the field.
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