Temp of a Comm Satellite in Orbit Around Earth

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SUMMARY

Satellites in orbit around Earth experience extreme temperature variations, reaching over 300°F on the sunlit side and nearly as low as -300°F on the shaded side. The core temperature of communication satellites averages around Earth surface temperature, fluctuating within ±30°C due to sophisticated thermal control systems that manage heat through radiation. Without these systems, the final temperature of an object in space would depend on its material properties, orbital geometry, and spin rates, ranging from 4K to the temperature of the Sun.

PREREQUISITES
  • Understanding of thermal dynamics in space environments
  • Familiarity with satellite thermal control systems
  • Knowledge of radiation heat transfer principles
  • Basic concepts of orbital mechanics
NEXT STEPS
  • Research satellite thermal control systems and their components
  • Study the principles of radiation heat transfer in vacuum
  • Learn about the effects of orbital geometry on satellite temperatures
  • Explore materials used in satellite construction and their thermal properties
USEFUL FOR

Aerospace engineers, satellite designers, thermal analysts, and anyone involved in the development or operation of communication satellites will benefit from this discussion.

MonstersFromTheId
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My understanding is that pretty much anything in orbit of Earth is subjected to some, to say the least, "extreme" temperatures. 300F degrees or more above zero on the sunny side, and dammed near as much below zero on the shady side.

So what's the average temp at the core of something like a Comm satellite?
 
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spin to avg temps?
 
Temperature in space is very non-intuitive.

Remember, there is no air, and most of the heat we're used to is transferred via conduction from the air which surrounds us.

The only way for a satellite to get hot is through radiation from the Sun or the Earth. The only way for it to get cold is through radiation to the background or the Earth.

Real satellites use complicated thermal systems to pump heat around to radiative panels to get rid of it, so any internal components are more-or-less at Earth surface temperature plus-or-minus about 30 degrees C.

If you just had a block of stuff in space with no thermal control system whatsoever, the final temperature would depend on the absorption and emmission properties of the material, how long the Earth occludes light from the Sun during the object's orbit, geometry and spin rates, etc... so somewhere between 4K and the temperature of the Sun.
 

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