Calculating radius in circular motion without frequency or force?

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SUMMARY

The discussion focuses on calculating the orbital radius of a 4400.0 kg satellite around Mars, which orbits at a speed of 2645.0 m/s. Key parameters include Mars' mass (6.4191 x 1023 kg), radius (3.397 x 106 m), and the gravitational constant (G = 6.67428 x 10-11 N-m2/kg2). The solution involves applying the universal law of gravitation to determine the necessary centripetal force for circular motion, ultimately leading to the calculation of the orbital radius from the center of Mars.

PREREQUISITES
  • Understanding of circular motion and centripetal force
  • Familiarity with the universal law of gravitation
  • Basic knowledge of kinematic equations
  • Ability to manipulate algebraic equations
NEXT STEPS
  • Study the derivation of the centripetal force equation in circular motion
  • Learn how to apply the universal law of gravitation in orbital mechanics
  • Explore the relationship between orbital speed and radius
  • Investigate the effects of varying mass and speed on satellite orbits
USEFUL FOR

Students in physics, aerospace engineers, and anyone interested in orbital mechanics and satellite dynamics will benefit from this discussion.

InertialRef
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Homework Statement



Scientists want to place a 4400.0 kg satellite in orbit around Mars. They plan to have the satellite orbit at a speed of 2645.0 m/s in a perfectly circular orbit. Here is some information that may help solve this problem:

mmars = 6.4191 x 1023 kg
rmars = 3.397 x 106 m
G = 6.67428 x 10-11 N-m2/kg2

What radius should the satellite move at in its orbit? (Measured from the center of Mars.)

Homework Equations



v = 2∏r/T

The Attempt at a Solution



This question makes no sense. Is there any way to calculate the period of the motion using a different equation? Otherwise, there are two unknowns, irrespective of which equation is used. Even if I attempt to use two different equations that are solved for T and equate them, there is always an unknown such as frequency or acceleration present along with radius.
 
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InertialRef said:

Homework Statement



Scientists want to place a 4400.0 kg satellite in orbit around Mars. They plan to have the satellite orbit at a speed of 2645.0 m/s in a perfectly circular orbit. Here is some information that may help solve this problem:

mmars = 6.4191 x 1023 kg
rmars = 3.397 x 106 m
G = 6.67428 x 10-11 N-m2/kg2

What radius should the satellite move at in its orbit? (Measured from the center of Mars.)

Homework Equations



v = 2∏r/T

The Attempt at a Solution



This question makes no sense. Is there any way to calculate the period of the motion using a different equation? Otherwise, there are two unknowns, irrespective of which equation is used. Even if I attempt to use two different equations that are solved for T and equate them, there is always an unknown such as frequency or acceleration present along with radius.

If the object is moving in a *circle*, then just as a kinematic requirement, what kind of force must be acting on it? What physical force in this problem is acting as that force (that keeps it moving in a circle)?
 
Ahh, universal law of gravitation. Okay, I think I might have a handle on this. Thank you.
 

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