Equation for Final velocity: Projectile Fired from Earth

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SUMMARY

The discussion centers on the calculation of final velocity for a projectile fired from Earth with an initial speed of 12.0 km/s, exceeding escape velocity. The correct energy conservation equation is established as 1/2 m vi2 - GME/RE = 1/2 m vf2, where G is the gravitational constant, ME is the mass of Earth, and RE is the radius of Earth. At infinite separation, the potential energy approaches zero, allowing for the simplification of the equation. The discussion also touches on calculating velocity at a distance of 4 Earth radii above the surface.

PREREQUISITES
  • Understanding of kinetic and potential energy concepts
  • Familiarity with gravitational constant (G) and mass of Earth (ME)
  • Knowledge of energy conservation principles in physics
  • Basic understanding of projectile motion and escape velocity
NEXT STEPS
  • Study the derivation of gravitational potential energy equations
  • Learn about energy conservation in non-uniform gravitational fields
  • Explore the concept of escape velocity in different celestial contexts
  • Investigate the effects of altitude on gravitational force and potential energy
USEFUL FOR

Physics students, aerospace engineers, and anyone interested in the dynamics of projectile motion and gravitational effects on objects launched from Earth.

sweetpete28
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Suppose a projectile is fired upward from the surface of the Earth. If the initial speed of the projectile is v = 12.0 km/s (more than the escape velocity): how fast will it be moving it is so far from Earth that the force of gravity is approximately zero?

The equation I was given to solve is:

1/2 v(initial)^2 - G(Mass of Earth) / radius of Earth = 1/2v(final)^2

I do NOT think this equation is correct. Can someone please help/advise? Many thanks.
 
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sweetpete28 said:
Suppose a projectile is fired upward from the surface of the Earth. If the initial speed of the projectile is v = 12.0 km/s (more than the escape velocity): how fast will it be moving it is so far from Earth that the force of gravity is approximately zero?

The equation I was given to solve is:

1/2 v(initial)^2 - G(Mass of Earth) / radius of Earth = 1/2v(final)^2

I do NOT think this equation is correct. Can someone please help/advise? Many thanks.

"so far from Earth that the force of gravity is approximately zero" means basically at infinite separation.

At all times, the sum of Kinetic and Potential energy is constant.

Kinetic energy is given by 1/2 m v2

Potential energy is given by -GMEm/R

when r = ∞ , Potential Energy = zero

thus comparing "at the surface" - the initial position - to infinite separation - the final position - we have

1/2 m vi2 + -GMEm/RE = 1/2 m vf2

Once you cancel the common term - the mass of the satellite - you get the equation you were given.

As an aside:
If you wanted to find out how fast it was traveling 4 Earth radii above the surface [which means a centre - centre separation of 5RE] you would use:

1/2 m vi2 + -GMEm/RE = 1/2 m vf2+ -GMEm/5RE
 

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