How Does Charge Buildup Affect Satellites in Earth's Radiation Belts?

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Homework Help Overview

The discussion revolves around the effects of charge buildup on satellites as they traverse Earth's radiation belts, specifically focusing on a spherical metallic satellite that accumulates charge during its orbit. The problem involves calculating surface charge density and the electric field due to this charge.

Discussion Character

  • Exploratory, Assumption checking, Mathematical reasoning

Approaches and Questions Raised

  • Participants discuss the calculation of surface charge density using the formula for charge per unit area. There is a mention of confusion regarding the correct area to use for a sphere versus a circle, indicating a need for clarification on geometric considerations.

Discussion Status

Some participants have offered guidance regarding the correct formula to use for the surface area of a sphere, suggesting that the original poster may have overlooked this aspect. The discussion is ongoing, with participants actively engaging in clarifying the approach to the problem.

Contextual Notes

There is an indication that the original poster is struggling with the calculations and assumptions related to the geometry of the satellite, which may affect their understanding of the problem. No explicit consensus has been reached yet.

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Space vehicles traveling through Earth's radiation belts can intercept a significant number of electrons. The resulting charge buildup can damage electronic components and disrupt operations. Suppose a spherical metallic satellite 0.9 m in diameter accumulates 2.2 µC of charge in one orbital revolution.
(a) Find the resulting surface charge density.
C/m2
(b) Calculate the magnitude of the electric field just outside the surface of the satellite, due to the surface charge.
N/C

Homework Equations


a. Looking at the units I need the answer in, I assumed that the surface charge density is charge/area or C/m^2.
for this problem that would be Q /(pie x r^2) or 2.2e^-6C / (pie x .45^2)

So I solved and got 2.2e-6/.6361725124 = 3.458e-6

This is not the right answer - I can't find part a which should be easy - a little help please.
 
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Laxman2974 said:
a. Looking at the units I need the answer in, I assumed that the surface charge density is charge/area or C/m^2.
for this problem that would be Q /(pie x r^2) or 2.2e^-6C / (pie x .45^2)

So I solved and got 2.2e-6/.6361725124 = 3.458e-6

This is not the right answer - I can't find part a which should be easy - a little help please.

The satellite is spherical in shape.

The area you have is the area of a circle, not the surface area of a sphere...
 
wow - thanks - I knew there was something obvious I was over looking
 
Laxman2974 said:
wow - thanks - I knew there was something obvious I was over looking

No problem. Glad I could help.:smile:
 

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