Home
Class 11
PHYSICS
Assuming that earth and mars move in cir...

Assuming that earth and mars move in circular orbits around the sun, with the martian orbit being 1.52 times the orbital radius of the earth. The length of the martian year is days is

A

`(1.52)^(2//3)xx365`

B

`(1.52)^(3//2)xx365`

C

`(1.52)^(2)xx365`

D

`(1.52)^(3)xx365`

Text Solution

AI Generated Solution

The correct Answer is:
To find the length of the Martian year in days, we can use Kepler's third law of planetary motion. Here's a step-by-step solution: ### Step 1: Understand Kepler's Third Law Kepler's third law states that the square of the orbital period (T) of a planet is directly proportional to the cube of the semi-major axis (a) of its orbit. Mathematically, this is expressed as: \[ T^2 \propto a^3 \] This can be written as: \[ \frac{T_m^2}{T_e^2} = \frac{a_m^3}{a_e^3} \] Where: - \( T_m \) = orbital period of Mars - \( T_e \) = orbital period of Earth - \( a_m \) = orbital radius of Mars - \( a_e \) = orbital radius of Earth ### Step 2: Define the Known Values From the problem, we know: - The orbital radius of Mars is 1.52 times that of Earth: \[ a_m = 1.52 \times a_e \] - The orbital period of Earth is: \[ T_e = 365 \text{ days} \] ### Step 3: Substitute the Known Values into Kepler's Law Using the relationship between the orbital radii, we can substitute \( a_m \) into Kepler's law: \[ \frac{T_m^2}{T_e^2} = \frac{(1.52 \cdot a_e)^3}{a_e^3} \] This simplifies to: \[ \frac{T_m^2}{T_e^2} = (1.52)^3 \] ### Step 4: Solve for \( T_m \) Now, we can express \( T_m \) in terms of \( T_e \): \[ T_m^2 = (1.52)^3 \cdot T_e^2 \] Taking the square root of both sides gives us: \[ T_m = T_e \cdot (1.52)^{3/2} \] ### Step 5: Substitute \( T_e \) to Find \( T_m \) Now, substituting \( T_e = 365 \) days: \[ T_m = 365 \cdot (1.52)^{3/2} \] ### Step 6: Calculate \( (1.52)^{3/2} \) First, calculate \( (1.52)^{3/2} \): 1. Calculate \( 1.52^{3} \): \[ 1.52^3 \approx 3.51 \] 2. Calculate \( (1.52)^{3/2} \): \[ (1.52)^{3/2} \approx \sqrt{3.51} \approx 1.87 \] ### Step 7: Final Calculation Now, substitute back into the equation for \( T_m \): \[ T_m \approx 365 \cdot 1.87 \approx 683.55 \text{ days} \] ### Conclusion Thus, the length of the Martian year is approximately **684 days**. ---

To find the length of the Martian year in days, we can use Kepler's third law of planetary motion. Here's a step-by-step solution: ### Step 1: Understand Kepler's Third Law Kepler's third law states that the square of the orbital period (T) of a planet is directly proportional to the cube of the semi-major axis (a) of its orbit. Mathematically, this is expressed as: \[ T^2 \propto a^3 \] This can be written as: ...
Promotional Banner

Topper's Solved these Questions

  • GRAVITATION

    NCERT FINGERTIPS ENGLISH|Exercise Universal law of Gravitations|14 Videos
  • GRAVITATION

    NCERT FINGERTIPS ENGLISH|Exercise The Gravitational constant|8 Videos
  • KINETIC THEORY

    NCERT FINGERTIPS ENGLISH|Exercise Assertion And Reason|10 Videos

Similar Questions

Explore conceptually related problems

The planet Mars has two moons. Phobos and Delmos (i) phobos has period 7 hours, 39 minutes and an orbital radius of 9.4 xx 10^(3) km . Calculate the mass of Mars. (ii) Assume that Earth and mars move in a circular orbit around the sun, with the martian orbit being 1.52 times the orbital radius of the Earth. What is the length of the martian year in days? (G = 6.67 xx 10^(-11) Nm^(2) kg^(-2))

Earth completes one orbit around the sun is

Assume that Earth is in circular orbit around the Sun with kinetic energy K and potential energy U, taken to be zero for infinite separation. Then, the relationship between K and U:

For a satellite moving in a circular orbit around the earth, the ratio of its potential energy to kinetic energy is

A satellite of Sun is in a circular orbit around the Sun, midway between the Suna and earth. Find the period of this satellite.

In adjoining figure earth goes around the sun in eliptical orbit on which point the orbital speed is maximum :

An artificial satellite moving in a circular orbit around the earth has a total energy E_(0) . Its potential energy is

For a satellite moving in a circular orbit around the earth, the ratio of its total mechanical energy to kinetic energy

An artificial satellite moving in a circular orbit around the earth has a total energy E_(0) . Its potential energy is

Two identical satellites are orbiting are orbiting at distances R and 7R from the surface of the earth, R being the radius of the earth. The ratio of their

NCERT FINGERTIPS ENGLISH-GRAVITATION-Assertion And Reason
  1. Assuming that earth and mars move in circular orbits around the sun, w...

    Text Solution

    |

  2. Assertion: The planet move slower when they are farther from the Sun t...

    Text Solution

    |

  3. Assertion : A central force is such that the force on the planet is al...

    Text Solution

    |

  4. Assertion: The motion of a particle under the central force is always ...

    Text Solution

    |

  5. Assertion: The time period of revolution of a satellite close to surfa...

    Text Solution

    |

  6. Assertion: When distance between bodies is doubled and also mass of ea...

    Text Solution

    |

  7. Assertion : The principle of superposition is not valid for gravitat...

    Text Solution

    |

  8. Assertion: The gravitational force on a particle inside a spherical sh...

    Text Solution

    |

  9. Assertion : Gravitational force between two masses in air is F. If the...

    Text Solution

    |

  10. Assertion: A man in a dosed cabin falling freely does not experience g...

    Text Solution

    |

  11. Assertion : For a free falling object, the next external force is just...

    Text Solution

    |

  12. Assertion: The total energy of a satellite is negative. Reason: Gra...

    Text Solution

    |

  13. Assertion : Moon has no atmosphere. Reason : The escape velocity fo...

    Text Solution

    |

  14. Assertion : The gravitational attraction of moon is much less than th...

    Text Solution

    |

  15. Assertion: A person sitting in an artificial satellite revolving aroun...

    Text Solution

    |

  16. Assertion : Geostationary satellites appear fixed from any point on ea...

    Text Solution

    |