Home
Class 11
PHYSICS
A satellite is orbiting the earth in an ...

A satellite is orbiting the earth in an orbit with a velocity `4 km//s`, then the acceleration due to gravity at that height is (in `ms^(-2)`)

A

`0.4`

B

`0.62`

C

`0.87`

D

`1.21`

Text Solution

AI Generated Solution

The correct Answer is:
To find the acceleration due to gravity at the height where a satellite is orbiting the Earth with a velocity of 4 km/s, we can use the relationship between gravitational force and centripetal acceleration. ### Step-by-step Solution: 1. **Convert the velocity to meters per second**: The velocity of the satellite is given as 4 km/s. \[ v = 4 \text{ km/s} = 4 \times 10^3 \text{ m/s} \] 2. **Use the formula for centripetal acceleration**: The centripetal acceleration \( a_c \) of the satellite can be expressed as: \[ a_c = \frac{v^2}{r} \] where \( r \) is the distance from the center of the Earth to the satellite. 3. **Relate centripetal acceleration to gravitational acceleration**: The gravitational force provides the necessary centripetal force for the satellite's orbit. Thus, we have: \[ a_c = g' = \frac{GM}{r^2} \] where \( g' \) is the acceleration due to gravity at the height of the satellite, \( G \) is the universal gravitational constant, and \( M \) is the mass of the Earth. 4. **Set the equations equal**: Since both expressions represent the acceleration at the height of the satellite, we can set them equal to each other: \[ \frac{v^2}{r} = \frac{GM}{r^2} \] 5. **Rearranging the equation**: Multiply both sides by \( r^2 \): \[ v^2 \cdot r = GM \] Now, we can express \( g' \) in terms of \( v \): \[ g' = \frac{v^2}{r} \] 6. **Substituting the values**: We need to find \( r \). We can rearrange the equation to find \( r \): \[ r = \frac{GM}{v^2} \] However, we can also express \( g' \) in terms of known values. The radius of the Earth \( R \) is approximately \( 6.37 \times 10^6 \) m, and the gravitational acceleration at the surface \( g \) is approximately \( 9.81 \, \text{m/s}^2 \). 7. **Calculate \( g' \)**: Using the formula: \[ g' = \frac{v^2}{R} \] We can substitute \( v = 4 \times 10^3 \text{ m/s} \): \[ g' = \frac{(4 \times 10^3)^2}{6.37 \times 10^6} \] \[ g' = \frac{16 \times 10^6}{6.37 \times 10^6} \approx 2.51 \, \text{m/s}^2 \] 8. **Final Calculation**: After calculating, we find that the acceleration due to gravity at that height is approximately \( 2.51 \, \text{m/s}^2 \). ### Final Answer: The acceleration due to gravity at that height is approximately \( 2.51 \, \text{m/s}^2 \).

To find the acceleration due to gravity at the height where a satellite is orbiting the Earth with a velocity of 4 km/s, we can use the relationship between gravitational force and centripetal acceleration. ### Step-by-step Solution: 1. **Convert the velocity to meters per second**: The velocity of the satellite is given as 4 km/s. \[ v = 4 \text{ km/s} = 4 \times 10^3 \text{ m/s} ...
Doubtnut Promotions Banner Mobile Dark
|

Topper's Solved these Questions

  • GRAVITATION

    NARAYNA|Exercise LEVEL-V|54 Videos
  • GRAVITATION

    NARAYNA|Exercise LEVEL-VI|42 Videos
  • GRAVITATION

    NARAYNA|Exercise LEVEL -I(H.W)|56 Videos
  • FRICTION

    NARAYNA|Exercise Passage type of questions I|6 Videos
  • KINETIC THEORY OF GASES

    NARAYNA|Exercise LEVEL-III(C.W)|52 Videos

Similar Questions

Explore conceptually related problems

A satellite is revolving around the orbit with a tangential velocity of 6.4 km/s . Determine the radius of the orbit of the satellite.

Two satellites of identical masses orbit the Earth at different heights. The ratio of their distance from the centre of earth is d : 1 and the ratio of the acceleration due to gravity at those heights is g : 1. Then the ratio of their orbital velocities is ________ .

Knowledge Check

  • A satellite is revolving around the earth in a circular orbit at an altitude h where the acceleration due to gravity is g'. If the earth is a sphere of radius R then the period of the satellite is give by

    A
    `T=2pi sqrt((h)/(g'))`
    B
    `T=2pi sqrt((R )/(g'))`
    C
    `T=2pi sqrt((R+h)/(g'))`
    D
    `T=2pi sqrt((R-h)/(g'))`
  • A satellite is moving in an orbit around the earth due to

    A
    Burning of fuel
    B
    gravitational attraction between sun and earth
    C
    ejection of gases from the exhaust of the satellite
    D
    gravitational attraction between earth and the satellite
  • If the means radius of earth is R , its angular velocity is omega and the acceleration due to gravity at the surface of the earth is g then the cube of the radius of the orbit of a satellite will be

    A
    `(Rg)/(omega^(2))`
    B
    `(R^(2)g)/(omega)`
    C
    `(R^(2)g)/(omega^(2))`
    D
    `(R^(2)omega)/g`
  • Similar Questions

    Explore conceptually related problems

    Two satellites of one metric ton and twelve metric tons masses are revolving around the Earth. The heights of these two satellites from the Earth are 1600 km and 25600 km, respectively. What is the ratio of their time periods and what is the ratio of the accelerations due to gravity at those heights? (Radius of the Earth = 6400km)

    A geostationary satellite orbits the earth at a height of nearly 36000 km. What is the potential due to earth's gravity at the site of this satellite (take the potential energy at oo to be zero). Mass of earth is 6xx10^(24)kg , radius of earth is 6400 km.

    The earth is a solid sphere of radius 6400 km, the value of acceleration due to gravity at a height 800 km above the surface of the earth is

    If mean radius of earth is R, its angular velocity is omega and the acceleration due to gravity at the surface of the earth is g . Then the cube of the radius of the orbit of geostationary satellite will be

    A satellite of mass m revolves around the earth of radius R at a height x from its surface. If g is the acceleration due to gravity on the surface of the earth, the orbital speed of the satellite is