#Atmospheric entry 🔥 occurs at the #Kármán line at an altitude of 100 km. The main heating 🌡️during controlled entry takes place at altitudes of 65 to 35 kilometres, peaking at 58 kilometres. Notable #atmospheric entry accidents : https://en.wikipedia.org/wiki/Atmospheric_entry#Notable_atmospheric_entry_accidents

#Starship testflight : 235 km altitude

Pictures : https://commons.wikimedia.org/wiki/File:Skip_reentry_trajectory.svg https://commons.wikimedia.org/wiki/File:Starship_SN20_getting_a_tile_inspection_(close-up)_(51432107025).jpg

Atmospheric entry - Wikipedia

When an object penetrates the #atmosphere at the crazy speeds of orbital mechanics, the air is compressed into a shockwave in front of the object and heats up to very high temperature 🌡️.

After colliding with our object, the air in the zone of the shockwave can achieve local temperature of several thousand to several tens of thousands of degrees. This has the effect of ripping electrons from atoms, #ionizing the matter, and causing it to enter into a #plasma phase https://spaceandscience.fr/en/blog/atmospheric-entry

Atmospheric entry, or how to brake without getting fried ?

@spaceflight actually, the point depends on the solar activity. A more energized atmosphere would result in a higher altitude, at which gravity gets overpowered by aerodynamics forces.

The Karman line is only for reference here, I suspect they use a calculated dynamic pressure for telling the autopilot when to begin adaptive control.

Talk:Atmospheric entry - Wikipedia

@spaceflight ouch, no. Just no.

Entry Interface (EI) is actually a completely different beast. AFAIR EI was even on about 130 km for Apollo, and typically 125 km for the Space Shuttle. Not sure about Soyuz, I would need to read my literature.

EI is the point through which the final orbit shall pass, as part of the deorbit flight planning. It is not the point at which reentry begins or even the autopilot switches from orbital to reentry mode.