Home
Class 12
PHYSICS
A comet of mass m moves in a highly elli...

A comet of mass m moves in a highly elliptical orbit around the sun of mass M the maximum and minium distacne of the comet from the centre of the sun are `r_(1)` and `r_(2)` respectively the magnitude of angular momentum of the comet with respect to the centre of sun is

A

`[(GM_(1))/(r_(1)+r_(2))]^(1//2)`

B

`[(GMmr_(1))/(r_(1)+r_(2))]^(1//2)`

C

`[(rGM^(2)r_(1)r_(2))/(r_(1)+r_(2))]^(1//2)`

D

`[(2GMm^(2)r_(1)r_(2))/(r_(1)+r_(2))]^(1//2)`

Text Solution

Verified by Experts

The correct Answer is:
D

Using law of conservatin of angular momentum at location A and B we get

`L=mv_(1)r_(1)=mv_(2)r_(2) rarr v_(2)=(v_(1)r_(1))/(r_(2))`
using the principla of conservation of total energy at A and B
`1/2 mv_(1)^(2)-(GMm)/(r_(1))=1/2mv_(2)^(2)-(GMm)/(r_(2))`
or `v_(2)^(2)-v_(1)^(2)=2 GM (1)/(r_(2))-(1)/(r_(1))`
Putting the values from Eq i Eq ii and solving we get
`rarr L=mv_(1)r_(1)=m[(2GMr_(1)r_(2))/(r(1)+r_(2))]^(1//2)`
Promotional Banner

Topper's Solved these Questions

  • GRAVITATION

    MHTCET PREVIOUS YEAR PAPERS AND PRACTICE PAPERS|Exercise Exercise 2|36 Videos
  • GRAVITATION

    MHTCET PREVIOUS YEAR PAPERS AND PRACTICE PAPERS|Exercise MHT CET Corner|20 Videos
  • GRAVITATION

    MHTCET PREVIOUS YEAR PAPERS AND PRACTICE PAPERS|Exercise MHT CET Corner|20 Videos
  • FRICTION IN SOLID AND LIQUIDS

    MHTCET PREVIOUS YEAR PAPERS AND PRACTICE PAPERS|Exercise EXERCISE 2 (Miscellaneous Problems)|24 Videos
  • INTERFERENCE AND DIFFRACTION OF LIGHT

    MHTCET PREVIOUS YEAR PAPERS AND PRACTICE PAPERS|Exercise MHT CET Corner|24 Videos

Similar Questions

Explore conceptually related problems

A planet of mass m revolves in elliptical orbit around the sun of mass M so that its maximum and minimum distance from the sun equal to r_(a) and r_(p) respectively. Find the angular momentum of this planet relative to the sun.

A planet of mass m is moving in an elliptical orbit about the sun (mass of sun = M). The maximum and minimum distances of the planet from the sun are r_(1) and r_(2) respectively. The period of revolution of the planet wil be proportional to :

A planet of mass m moves along an ellipse around the sun so that its maximum and minimum distance from the sun are equal to r_(1) and r_(2) respectively. Find the angular momentum of this planet relative to the centre of the sun. mass of the sun is M .

A planet of mass m moves along an ellipse around the Sun so that its maximum and minimum distances from the Sun are equal to r_1 and r_2 respectively. Find the angular momentum M of this planet relative to the centre of the Sun.

A planet of mass m moves around the Sun of mass Min an elliptical orbit. The maximum and minimum distance of the planet from the Sun are r_(1) and r_(2) , respectively. Find the relation between the time period of the planet in terms of r_(1) and r_(2) .

A planet of mass m moves along an ellipse around the sum of mass M so that its maximum and minimum distances from sum are a and b respectively. Prove that the angular momentum L of this planet relative to the centre of the sun is L=msqrt((2GGMab)/((a+b)))

The maximum and minimum distance of a comet from the sun are 14 xx 10^9 m and 7 xx 10^7 m respectively. If the maximum velocity of the comet is 5 xx10^2 km/sec, its minimum velcity will be:-

A planet of mass m is moving in an elliptical orbit around the sun of mass M . The semi major axis of its orbit is a, eccentricity is e . Find speed of planet V_(1) at perihelion P

A planet of mass m is moving in an elliptical orbit around the sun of mass M . The semi major axis of its orbit is a, eccentricity is e . Find speed of planet V_(2) at aphelion A .

A planet of mass moves alng an ellipes around the sun so that its maximum distance from the sum are equal to r_(1) and r_(2) respectively . Find the angular momenture L of this planet relative to the centre of the sun. [Hint :L Rember that at the maximum and minimum distance velocity is perpendicular to tthe position vectors of the planet . Apply the princples of conservation of angula r momenture and energy .]

MHTCET PREVIOUS YEAR PAPERS AND PRACTICE PAPERS-GRAVITATION -Exercise 1
  1. The period of revolution of planet A round from the sun is 8 times tha...

    Text Solution

    |

  2. Which of the following graphs between the square of the time period an...

    Text Solution

    |

  3. A comet of mass m moves in a highly elliptical orbit around the sun ...

    Text Solution

    |

  4. Kepler's third law states that square of period revolution (T) of a pl...

    Text Solution

    |

  5. A staellite in a circular orbit of raidus R has a period of 4h anoth...

    Text Solution

    |

  6. The time period of a satellite of earth is 5 hours. If the separation ...

    Text Solution

    |

  7. The ratio of mean distances of three planets from the sun are 0.5 : 1:...

    Text Solution

    |

  8. All planets move in elliptical orbits with the sun situtated at one ...

    Text Solution

    |

  9. Law of areas is valid for any

    Text Solution

    |

  10. For motiion of planets in ellipticla orbits around the sun the centra...

    Text Solution

    |

  11. The law of areas can be interpreted as

    Text Solution

    |

  12. Kepler 's law of periods as applied to motion of satellite around t...

    Text Solution

    |

  13. Which of the following statement is correct about satellites?

    Text Solution

    |

  14. A satellite S is moving in an elliptical orbit around the earth. The m...

    Text Solution

    |

  15. A satellite is placed in a circular orbit around the earth at such a ...

    Text Solution

    |

  16. The earth (mass =6xx10^(24)kg) revolves round the sun with an angular ...

    Text Solution

    |

  17. The orbital velocity of an artifical satellite in a cirular orbit abov...

    Text Solution

    |

  18. If total enrgy of satellite is E what is its potential enrgy

    Text Solution

    |

  19. A relay satellite transmits the television programme from one part of ...

    Text Solution

    |

  20. By what percent the energy of the satellite has to be increased to shi...

    Text Solution

    |