An 8000 kg satellite is launched from the surface of the Earth into outer space. What initial kinetic energy is needed by the satellite in order to reach a great (i.e., infinite) distance from the Earth, neglecting the effects of air resistance in the atmosphere? (G = 6.67 × 10-11 N-m²/kg², MẸ = 5.97 ×x 1024 kg, Rf = 6.37 × 106 m.) %3D Multiple Choice 5.00 x 1011 J. 4.03 x 1011 J. 3.57 x 1011 J.

An 8000 kg satellite is launched from the surface of the Earth into outer space. What initial kinetic energy is needed by the satellite in order to reach a great (i.e., infinite) distance from the Earth, neglecting the effects of air resistance in the atmosphere? (G = 6.67 × 10-11 N-m²/kg², MẸ = 5.97 ×x 1024 kg, Rf = 6.37 × 106 m.) %3D Multiple Choice 5.00 x 1011 J. 4.03 x 1011 J. 3.57 x 1011 J.

Principles of Physics: A Calculus-Based Text

5th Edition

ISBN:9781133104261

Author:Raymond A. Serway, John W. Jewett

Publisher:Raymond A. Serway, John W. Jewett

Chapter11: Gravity, Planetary Orbits, And The Hydrogen Atom

Section: Chapter Questions

Problem 30P

See similar textbooks

Similar questions

A space probe is fired as a projectile from the Earths surface with an initial speed of 2.00 104 m/s. What will its speed be when it is very far from the Earth? Ignore atmospheric friction and the rotation of the Earth. P11.26 Ki+Ui=Kf+Uf12mvi2+GMEm(1rf1ri)=12mvf212vi2+GME(01RE)=12vf2orvf2=v122GMEREandvf=(v122GMERE)1/2,vf=[(2.00104)21.25108]1/2m/s=1.66104m/s
A system consists of five particles. How many terms appear in the expression for the total gravitational potential energy of the system? (a) 4 (b) 5 (c) 10 (d) 20 (e) 25
Find the escape speed of a projectile from the surface of Jupiter.
Rank the following quantities of energy from largest to the smallest. State if any are equal. (a) the absolute value of the average potential energy of the SunEarth system (b) the average kinetic energy of the Earth in its orbital motion relative to the Sun (c) the absolute value of the total energy of the SunEarth system
If a spacecraft is headed for the outer solar system, it may require several gravitational slingshots with planets in the inner solar system. If a spacecraft undergoes a head-on slingshot with Venus as in Example 11.6, find the spacecrafts change in speed vS. Hint: Venuss orbital period is 1.94 107 s, and its average distance from the Sun is 1.08 1011 m.
An 8000 kg satellite is launched from the surface of the Earth into outer space. What initial kinetic energy is needed by the satellite in order to reach a great (i.e., infinite) distance from the Earth, neglecting the effects of air resistance in the atmosphere? (G = 6.67 × 10−11 N·m2/kg2, ME = 5.97 × 1024 kg, RE = 6.37 × 106 m.)
A satellite has a mass of 5850 kg and is in a circular orbit 4.10 × 105 m above the surface of a planet. The period of the orbit is 2.00 hours. The radius of the planet is 4.15 × 106 m. (a) Find the mass of the planet,(b) the energy of the orbit, and (c) the escape velocity from this orbit. If the speed of the satellite is increased by 20% what would be the maximum distance above the planet? Needs Complete typed solution with 100% accuracy.
A spaceship with m = 1.00 ✕ 104 kg is in a circular orbit around the Earth, h = 800 km above its surface. The ship's captain fires the engines in a direction tangent to the orbit, and the spaceship assumes an elliptical orbit around the Earth with an apogee of d = 3.00 ✕ 104 km, measured from the Earth's center. How much energy (in J) must be used from the fuel to achieve this orbit? (Assume that all the fuel energy goes into increasing the orbital energy and that the perigee distance is equal to the initial radius.)
If the mass and radius of Mars are 6.39 × 1023 kg and 3.4 × 106 m, respectively, what is the escape velocity needed for a spaceship of mass 25,000 kg to escape the gravitational potential well of Mars? A) 1,200 m/s B). 8,658 m/s C). 7,270 m/s D). 5,022 m/s
If you wanted to place a satellite in a geosynchronous orbit, at what height above the Earth's surface should you place it? (Earth's mass = 5.98x10^24, Earth's radius = 6x10^6, G = 6.67x10^-11) For the previous situation using the given answer, what is the difference in potential energy between the Earth's surface and the satellite height for a satellite with 1 kg mass?
A 1500 kg satellite is in a stable orbit at an altitude of 4.0 × 10 5 m above Earth's surface. What is the satellite's total energy in this orbit? (Mearth = 5.97x1024 kg) (rearth = 6.4x106 m)
A 1950 kg weather satellite moves in a circular orbit with a gravitational potential energy of 1.69 x 1015 J with respect to Earth’s surface. At its location, free-fall acceleration is only 6.44 m/s2 . How high above Earth’s surface is the satellite?