मराठी
तामिळनाडू बोर्ड ऑफ सेकेंडरी एज्युकेशनएस.एस.एल.सी. (इंग्रजी माध्यम) इयत्ता ९

The third law of Kepler is also known as the Law of ______.

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प्रश्न

The third law of Kepler is also known as the Law of ______.

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उत्तर

The third law of Kepler is also known as the Law of Harmonies 5.8.

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पाठ 9: Universe - Exercise [पृष्ठ १११]

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सामाचीर कलवी Science [English] Class 9 TN Board
पाठ 9 Universe
Exercise | Q II. 4. | पृष्ठ १११

संबंधित प्रश्‍न

State Kepler's law of orbit and law of equal areas.


Identify the law shown in the figure and state three respective laws.


Answer the following question.

State Kepler’s law of the period.


Write the Kepler’s laws.


If the distance between the sun and the earth is made three times, then attraction between the two will ______


A planet is revolving around the sun in an elliptical orbit as shown in figure. At which point will its K.E. be maximum?


The centre of mass of an extended body on the surface of the earth and its centre of gravity ______.

  1. are always at the same point for any size of the body.
  2. are always at the same point only for spherical bodies.
  3. can never be at the same point.
  4. is close to each other for objects, say of sizes less than 100 m.
  5. both can change if the object is taken deep inside the earth.

Out of aphelion and perihelion, where is the speed of the earth more and why?


A star like the sun has several bodies moving around it at different distances. Consider that all of them are moving in circular orbits. Let r be the distance of the body from the centre of the star and let its linear velocity be v, angular velocity ω, kinetic energy K, gravitational potential energy U, total energy E and angular momentum l. As the radius r of the orbit increases, determine which of the above quantities increase and which ones decrease.


A satellite is in an elliptic orbit around the earth with aphelion of 6R and perihelion of 2 R where R= 6400 km is the radius of the earth. Find eccentricity of the orbit. Find the velocity of the satellite at apogee and perigee. What should be done if this satellite has to be transferred to a circular orbit of radius 6R ?

[G = 6.67 × 10–11 SI units and M = 6 × 1024 kg]


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