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Questions tagged [thermal]

How heat affects spacecraft and space missions, or materials and methods to deal with heat.

6 votes
1 answer
688 views

Shielding against hypervelocity impacts is a thing, like a whipple shield. Easy enough for many things, like various habitat modules. But radiators are required to be very large in size, particularly ...
AlanSE's user avatar
  • 16.6k
5 votes
1 answer
145 views

As plans for long-term lunar habitation (such as the Artemis program) progress, the need for scalable power distribution—likely involving AC microgrids—becomes critical. However, standard terrestrial ...
Andi Pangerang Hasanuddin's user avatar
1 vote
1 answer
169 views

Are there any available data on the Space Shuttle External Tank wall temperatures, for the points and surfaces other than the stagnation point? I found an interesting paper here -> https://ntrs....
Irocket's user avatar
  • 171
1 vote
2 answers
340 views

I am working on a school project for a 3U Cubesat, specifically the thermal control subsystem. First, I would like to calculate the internal temperature of a "satellite" (assuming the "...
Marcus Sten's user avatar
2 votes
1 answer
87 views

Did the Shields-1 cubesat have multilayer insulation outside the surface for thermal protection?
Arjun Krishnan's user avatar
2 votes
1 answer
181 views

I imagine the surface of Europa to be a barren atmospheric wasteland. But under the ice, acting as insulation, and where water meets soil, would it be warmer from geothermic heat to better support ...
Justintimeforfun's user avatar
2 votes
0 answers
61 views

I am aware that increased emissivity in solar sails aids with heat reduction, however, I have done some research and found that the emissivity decreases the trajectory of the solar sail through the ...
holly newman's user avatar
6 votes
0 answers
223 views

I have a simulation that describes a vehicle traveling at very high speeds (near or even above orbital) up out of the atmosphere and into space. I'd like to chart the rate of heating ($\dot{q}_{conv}$ ...
phil1008's user avatar
  • 9,443
2 votes
1 answer
2k views

If paired with tile density information, this total volume information would be useful for estimating how much more mass Starship could lift in a non-reusable configuration. If also paired with heat ...
phil1008's user avatar
  • 9,443
8 votes
2 answers
3k views

I'm curious about images (or videos) that a) Include both a portion of the vehicle and its re-entry plasma wake, and b) That were taken at near-orbital (high-hypersonic) velocities or greater. I ...
phil1008's user avatar
  • 9,443
2 votes
1 answer
391 views

I suspect that the white padding material between the tile and the stainless steel skin might be [Nomex Felt][1], but I don't really know. Nomex was used on the Space Shuttle. Flame-Resistant Felt - ...
phil1008's user avatar
  • 9,443
2 votes
0 answers
429 views

Are tiles that much more cost effective as a thermal protection system? What other novel methods have been tried? The obvious issues seem to be different thermal properties and rigidity and how to ...
Dagelf's user avatar
  • 733
3 votes
2 answers
2k views

I bumped into a question regarding LEO orbit. Is an external temperature profile available in literature as a first approximation for thermal analysis? I bumped into articles mentioning that the ...
Enrico's user avatar
  • 31
5 votes
1 answer
324 views

Yesterday, I asked a question about the square-cube law and propellant tanks. Do larger rockets tend to have a better mass ratio due to the square cube law? I have a very similar question about ...
Krzysiek's user avatar
  • 153
2 votes
0 answers
890 views

Just as the title, how could one find out, or simply estimate the maximum and minimum likely surface temperatures of a satellite orbiting in GEO.
parry's user avatar
  • 21

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