Centripetal Acceleration Part II

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SUMMARY

The discussion focuses on calculating the time required for a satellite to complete one orbit given its speed and the radius of its orbit. Using the centripetal acceleration formula and the gravitational constant (G = 6.67259e-11) along with Earth's mass (5.98e24 kg), the satellite's speed is determined to be 7723.55 m/s. The correct orbital period (T) is derived using the equation v = 2πr/T, resulting in T = 5221.57 seconds, which converts to approximately 1.51155 hours.

PREREQUISITES
  • Understanding of centripetal acceleration and its relationship to orbital motion
  • Familiarity with the gravitational constant (G) and Earth's mass
  • Knowledge of the formula v = 2πr/T for circular motion
  • Ability to perform unit conversions, particularly from seconds to hours
NEXT STEPS
  • Study the implications of centripetal acceleration in satellite dynamics
  • Learn about gravitational forces and their effect on orbital mechanics
  • Explore the derivation of orbital period formulas for different celestial bodies
  • Investigate the effects of varying orbital radii on satellite speed and period
USEFUL FOR

Students studying physics, particularly those focusing on mechanics and orbital dynamics, as well as educators looking for examples of satellite motion calculations.

BitterSuites
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[SOLVED] Centripetal Acceleration Part II

Homework Statement



(From previous question) In order for a satellite to move in a stable circular orbit of radius 6689 km at a constant speed, its centripetal acceleration must be inversely proportional to the square of the radius of the orbit.

What is the speed of the satellite? The G is 6.67259e-11 and the mass of the Earth is 5.98e24kg.

The answer to this was 7723.55 m/s.

Part II:

Find the time required to complete one orbit. Answer in units of h.

Homework Equations



The book only gives one equation for T referencing orbits, which is v=2pir/T

The Attempt at a Solution



v=2pi/T
7723.55 = 2pi/T
7723.55T = 2pi
T = 2pi/7723.55
T = .000814

I think the homework system even laughed at me when I entered that answer :)
 
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BitterSuites said:

Homework Equations



The book only gives one equation for T referencing orbits, which is v=2pir/T
Right.

The Attempt at a Solution



v=2pi/T
Wrong.

Compare the two equations. (You left off the r.)

And don't forget to convert your answer to the desired units.
 
*sigh* I keep making really silly mistakes.

So I input the correct equation but it came out correct.

v=2pir/t
7723.55 m/s = 2pi * 6689000m/T
7723.55T = 4.20282e7
T = 5221.57 seconds

Convert to hours

5221.57/60 = 90.6928 minutes
90.6928/60 = 1.51155 hours

Thank you so much.
 
Last edited:

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