Temperature of the surface of a satellite?

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SUMMARY

The temperature of a satellite's surface varies significantly based on several factors, including its orientation to the Sun, the emissivity and reflectivity of its materials, and internal heat generation from components like batteries and solar panels. The surface can reach extreme temperatures, similar to those of the Moon, depending on whether it is facing the Sun or not. Accurate temperature measurement requires the use of temperature sensors on the satellite, as theoretical calculations are complex and depend on multiple variables.

PREREQUISITES
  • Understanding of emissivity and reflectivity in thermal dynamics
  • Knowledge of satellite orientation and its impact on solar radiation exposure
  • Familiarity with internal heat generation mechanisms in satellites
  • Basic principles of the Stefan-Boltzmann law
NEXT STEPS
  • Research the Stefan-Boltzmann law and its applications in thermal analysis
  • Explore materials science focusing on emissivity and reflectivity properties
  • Learn about satellite thermal control systems and temperature sensor technologies
  • Investigate case studies of temperature management in space missions
USEFUL FOR

Aerospace engineers, thermal analysts, and students in mechanical or space engineering will benefit from this discussion, particularly those interested in satellite design and thermal management.

pixel01
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Anybody has an idea about that?

Thanks
 
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Are you asking what the temperature is? It depends on a lot of factors and there is no one answer.
 
Thanks for your answering.
May I thing of an estimate. Could it be as cold as the Moon surface? No atmosphere, the same distance to the Sun..
 
Yes, it could be as cold as the moon's surface -- or as hot as the moon's surface.
 
It's complicated depending on heat generation and transfer from the satellite.

The surface facing the sun can get quite hot, while the surface away from the sun can get quite cold.

Reflectivity and emissivity are two key factors affecting radiative energy transport.
 
I'm just a college freshman, but if you think about it, there are so many factors that can affect this. It depends on how much heat the material of the satellite's surface absorbs and reflects. Also, it depends whether it is facing the sun with or without the obstruction of another satellite or heavenly body. There is really no way to "calculate" this; the only way to do it is to use a temp sensor on the satellite itself. Good question, though, it got me awake and thinking this morning.
 
Knowing the materials used to cover the satellite helps, also its distance fom the sun and its proximity to the earth.
Its a classic Stephan Boltzmann thingy - Joe Satrianni has got the idea.
Reflectivity and Emissivity. - Nicely done Joe
 
hey pixel,

i covered this stuff in a final year mechanical and space engineering degree and there is an equation that exists to work it out, however finding that equation is quite difficult. i have it buried somewhere in my old notes somewhere and if i can be bothered finding it when i get home i'll let you know.

a quick answers is that it isn't cold at all, it depends on several factors. I will try to list them;

- the emissivity and reflectivity of the satellite material
- the orientation of the satelite to the sun which will determine the surface area exposed to the suns radiation
- internal heat generation of the satelite itself e.g. batteries, fuel cells, solar panels etc.
- distance from the sun
- there are a few constants chucked in there as well :S

i will try and remember to find the equation when i get home... you have me intrigued again :P
 

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