Determine Altitude from Constant Speed and Acceleration of Satellite S

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SUMMARY

The altitude of satellite S, which travels at a constant speed of 20 Mm/h (5555.6 m/s) with a centripetal acceleration of 2.5 m/s², is calculated using the formula for centripetal acceleration, a_n = v²/ρ. By rearranging this equation, the radius ρ is determined to be approximately 12,345,679.01 m. Subtracting the Earth's radius (6,356,500 m) from this value yields an altitude of approximately 5,989.18 km. The initial confusion arose from incorrectly using the Earth's diameter instead of its radius in the calculations.

PREREQUISITES
  • Understanding of centripetal acceleration and its formula a_n = v²/ρ
  • Knowledge of unit conversions, specifically from Mm/h to m/s
  • Familiarity with the Earth's dimensions, including its radius and diameter
  • Basic algebra skills for rearranging equations and performing calculations
NEXT STEPS
  • Study the principles of circular motion and centripetal acceleration in physics
  • Learn about unit conversions and their importance in scientific calculations
  • Explore the implications of altitude on satellite operations and orbital mechanics
  • Investigate the effects of gravitational forces on satellite trajectories
USEFUL FOR

Students in physics or engineering, satellite engineers, and anyone involved in orbital mechanics or satellite design will benefit from this discussion.

KillerZ
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Homework Statement



The satellite S travels around the Earth in a circular path with a constant speed of 20 Mm/h. If the acceleration is 2.5m/s2, determine the altitude h. Assume the Earth's diameter to be 12 713 km.

i5akx3.png


Homework Equations



a_{n}= \frac{v^{2}}{\rho}

The Attempt at a Solution



I thought that a_{t}= 0 because speed is constant and a_{n}= 20 Mm/h and I just solved the above equation for \rho but that came out to a negative number so that's not right.
 
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KillerZ said:

Homework Statement



The satellite S travels around the Earth in a circular path with a constant speed of 20 Mm/h. If the acceleration is 2.5m/s2, determine the altitude h. Assume the Earth's diameter to be 12 713 km.

i5akx3.png


Homework Equations



a_{n}= \frac{v^{2}}{\rho}

The Attempt at a Solution



I thought that a_{t}= 0 because speed is constant and a_{n}= 20 Mm/h and I just solved the above equation for \rho but that came out to a negative number so that's not right.
Why are you using the tangential speed as the acceleration? The acceleration is, as you have stated, a = v^2/r. But there is another expression for a as well, since the acceleration is provided by ...? Write the equation for that acceleration. With those two equations you should be able to solve for the two unknowns, a and r.

AM
 
Ops that was a typo. I meant a_{n}= 2.5 m/s^{2}
 
KillerZ said:
Ops that was a typo. I meant a_{n}= 2.5 m/s^{2}
Ok. I misread the question too. You are given the acceleration. What units must v have in your equation a_n = v^2/r?

AM
 
v should be m/s I think. Which I calculated 20 Mm/h = 5555.556 m/s
 
KillerZ said:
v should be m/s I think. Which I calculated 20 Mm/h = 5555.556 m/s
So what is r? How is r related to h?

AM
 
I am assuming r would be to the center of the Earth and h is r - the Earth's radius.
 
Ok I think I got this:

v = 20 Mm/h = 5555.6 m/s

a_{n} = 2.5 m/s^{2}

a_{n}= \frac{v^{2}}{\rho}

\rho= \frac{v^{2}}{a_{n}}

\rho= \frac{5555.6}{2.5} = 12345679.01 m


h = \rho - Earth's radius = 12345679.01 - 6356500 = 5989179.01 = 5989.18 km
 
that looks better now, I think you were getting a negative number because you were subtracting the diameter instead of the radius.
 
  • #10
Ya that's what I was doing.
 

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