Problem 59
Question
(II) A NASA satellite has just observed an asteroid that is on a collision course with the Earth. The asteroid has an estimated mass, based on its size, of \(5 \times 10^{9} \mathrm{~kg}\). It is approaching the Earth on a head-on course with a velocity of \(660 \mathrm{~m} / \mathrm{s}\) relative to the Earth and is now \(5.0 \times 10^{6} \mathrm{~km}\) away. With what speed will it hit the Earth's surface, neglecting friction with the atmosphere?
Step-by-Step Solution
Verified Answer
The asteroid will hit the Earth's surface with a speed of approximately 11180 m/s.
1Step 1: Convert Distance to Meters
First, convert the distance from kilometers to meters. The asteroid is currently \(5.0 \times 10^{6} \text{ km} = 5.0 \times 10^9 \text{ m}\).
2Step 2: Use Conservation of Energy
Use the conservation of energy to determine the final velocity of the asteroid. Initially, the asteroid has kinetic energy \(KE_i = \frac{1}{2}mv_i^2\) and gravitational potential energy \(U_i = -\frac{G M e m}{r_0}\), where \(M_e\) is the Earth's mass, \(r_0\) is the initial distance, and \(G\) is the gravitational constant.
3Step 3: Express Initial Energy
Calculate the initial total energy: \[ E_i = \frac{1}{2} m v_i^2 - \frac{G M_e m}{r_0} \] where \(m = 5 \times 10^9 \text{ kg}\), \(v_i = 660 \text{ m/s}\), \(G = 6.674 \times 10^{-11} \text{ m}^3 \text{ kg}^{-1} \text{ s}^{-2}\), \(M_e = 5.972 \times 10^{24} \text{ kg}\), and \(r_0 = 5.0 \times 10^9 \text{ m}\).
4Step 4: Express Final Energy
For final energy when the asteroid hits the Earth's surface: \[ E_f = \frac{1}{2} m v_f^2 - \frac{G M_e m}{R_e} \] where \(v_f\) is the final velocity and \(R_e = 6.371 \times 10^6 \text{ m}\) is the Earth's radius.
5Step 5: Solve Conservation Equation
Since energy is conserved \(E_i = E_f\) hence, \[ \frac{1}{2} m v_i^2 - \frac{G M_e m}{r_0} = \frac{1}{2} m v_f^2 - \frac{G M_e m}{R_e} \]Cancel mass \(m\) and solve for \(v_f\).
6Step 6: Calculate Final Velocity
Rearrange to find: \[ v_f = \sqrt{v_i^2 + 2 G M_e \left( \frac{1}{R_e} - \frac{1}{r_0} \right)} \]Substitute the values to find \(v_f \approx 11180 \text{ m/s}\).
Key Concepts
Conservation of EnergyGravitational Potential EnergyKinetic Energy
Conservation of Energy
In physics, the conservation of energy principle states that energy cannot be created or destroyed, although it can change forms. This concept is crucial in understanding how asteroids interact with Earth.
Consider an asteroid on a collision course with Earth. It possesses both kinetic and gravitational potential energy. As the asteroid gets closer, these energy types transform, but the total energy remains constant.
Consider an asteroid on a collision course with Earth. It possesses both kinetic and gravitational potential energy. As the asteroid gets closer, these energy types transform, but the total energy remains constant.
- Initial total energy = sum of initial kinetic energy and initial gravitational potential energy.
- Final total energy = sum of final kinetic energy and final gravitational potential energy at Earth's surface.
Gravitational Potential Energy
Gravitational potential energy (U) is the energy an object possesses because of its position in a gravitational field. For objects far from Earth or any massive body, it is defined as\[ U = -\frac{G M_em}{r} \]where:
- \(G\) is the gravitational constant.
- \(M_e\) is Earth's mass.
- \(m\) is the mass of the object, in this case, the asteroid.
- \(r\) is the distance from the object to the center of the Earth.
Kinetic Energy
Kinetic energy is the energy an object possesses due to its motion. It is given by the formula\[ KE = \frac{1}{2}mv^2 \]where:
- \(m\) is the mass of the object, which, for an asteroid, can be quite large.
- \(v\) is the speed of the object.
Other exercises in this chapter
Problem 56
(II) A meteorite has a speed of \(90.0 \mathrm{~m} / \mathrm{s}\) when \(850 \mathrm{~km}\) above the Earth. It is falling vertically (ignore air resistance) an
View solution Problem 57
(II) How much work would be required to move a satellite of mass \(m\) from a circular orbit of radius \(r_{1}=2 r_{\mathrm{E}}\) about the Earth to another cir
View solution Problem 60
(II) A sphere of radius \(r_{1}\) has a concentric spherical cavity of radius \(r_{2}\) (Fig. 40\()\) . Assume this spherical shell of thickness \(r_{1}-r_{2}\)
View solution Problem 61
(III) To escape the solar system, an interstellar spacecraft must overcome the gravitational attraction of both the Earth and Sun. Ignore the effects of other b
View solution