Physics for Scientists and Engineers
Physics for Scientists and Engineers
6th Edition
ISBN: 9781429281843
Author: Tipler
Publisher: MAC HIGHER
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Chapter 11, Problem 19P
To determine

Radius of the asteroid.

Expert Solution & Answer
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Answer to Problem 19P

Near about 3km

Explanation of Solution

Introduction:

The escape velocity on the surface of the asteroid is

  ve Asteroid=2GM asteroidR asteroid

Here, Masteroid is the mass of asteroid and Rasteroid is radius of asteroid.

Relation among mass, density and volume is ,

  M Asteroid=ρ AsteroidV Asteroid=ρ Asteroid43πR Asteroid3

The second kinematic equation of motion, vf2vi2=2gh

The escape velocity on the surface of the asteroid is

  ve Asteroid= 2G M asteroid R asteroid = 2G ρ  Asteroid 4 3 π R  Asteroid 3 R asteroid =( 8 3 πG ρ asteroid )Rasteroid....(1)

From the equation (1) ,

The radius of the Asteroid is given by

  Rasteroid=ve Asteroid38πGρ asteroid

From the kinematic equation of motion, vf2vi2=2gh

Here ‘h’ is the height to which you can jump on the surface of the Earth.

As finally come to rest, the final speed of you is v=0 m/s

Therefore

  vf2vi2=2gh0vi2=2ghvi=2gh

Let vi=ve asteroid

Therefore, the radius of the asteroid

  Rasteroid=ve Asteroid3 8πG ρ asteroid =2gh3 8πG ρ asteroid =3 8πG ρ asteroid ( gh)........(2)

Asssume that you can jump a height h=0.75 m , on the surface of Earth.

Density of the asteroid is ρAsteroid=(3.0 g/cm3)(1 kg1000 g)( 106  cm31  m3)

  =3.0×103 kg/m3

Universal gravitational constant is G=6.673×1011 N.m2/kg2

By substituting all known values in the equation (2) , we get

Radius of the asteroid is

  Rasteroid=3 8πG ρ asteroid ( 2gh)=3 8( 3.14 )( 6.73× 10 11  N .m 2 / kg 2 )( 3.0× 10 3 kg/m 3 )(2)( 9.8 m/s 2 )( 0.75 m)=(2.96× 103 m)( 1 km 1000 m)=3.0 km

Conclusion:

Radius of asteroid is 3 km

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(a) In order to keep a small satellite from drifting into a nearby asteroid, it is placed in orbit with a period of 3.02 hours and radius of 2.0 km. What is the mass of the asteroid? (b) Does this mass seem reasonable for the size of the orbit?
Example 4. A satellite is orbiting a circular orbit at an altitude of 900 km, at which atmosphere density is 5.46 x 10-13kg/m³. The satellite has mass 150kg, cross sectional area 1.50m², and drag coefficient 2. a) Calculate the rate of change of orbit radius da/dt in units of m/s. b) Make an estimate of the time (in years) that will take the satellite to reach the Earth.

Chapter 11 Solutions

Physics for Scientists and Engineers

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