Temperature

Space Shuttle re-entry plasma

Space Shuttle re-entry plasma is the extremely hot, ionised gas layer that forms around a spacecraft as it re-enters Earth's atmosphere at high speed.

Also known as: shuttle reentry plasma temperature

How big is it?

8,000 K

Representative plasma temperature · defined reference
Typical recorded range: 5,000 K to 10,000 K.

Scale illustration of Space Shuttle re-entry plasma, calibrated to its representative plasma temperature measurement.
The marked representative plasma temperature represents 8,000 K.

A little perspective

Space Shuttle re-entry plasma is 2,228 K warmer than Sun.

Sun: The Sun is the star at the centre of the Solar System.

Kelvin scale
THERMODYNAMIC TEMPERATURE · KELVIN8,000 K5,772 K0 K · absolute zero
01
Space Shuttle re-entry plasma8,000 KRepresentative plasma temperature
02
Sun5,772 KSurface temperature
Celsius and Fahrenheit zero points are offsets. Compare temperature differences, not ratios in °C or °F. The kelvin axis starts at absolute zero.
Measurements, assumptions & sources +

Space Shuttle re-entry plasma

An 8,000 K representative scale for the ionised shock-layer gas around a re-entering shuttle. Temperature varies strongly through the flow and is not the vehicle skin temperature.

Defined examples — our methodology

The marked representative plasma temperature is calibrated. Unmeasured illustration details are representative.

Sun

Our star, modelled with the IAU nominal solar radius. “Surface” means the visible photosphere. The core is much hotter; this is not a solid surface.

IAU — nominal solar and planetary conversion constants

The marked surface temperature is calibrated. Unmeasured illustration details are representative.

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Why this measurement?

Why we use 8,000 K

For comparison, this page uses representative plasma temperature. This is labelled defined reference: an explicit comparison model rather than a claim that every example has the same value. The recorded range is 5,000 K to 10,000 K.

An 8,000 K representative scale for the ionised shock-layer gas around a re-entering shuttle. Temperature varies strongly through the flow and is not the vehicle skin temperature.

The identifying illustration and the numerical comparison remain separate. How calibrated comparisons work →

Explore temperature →

Recorded properties

Space Shuttle re-entry plasma dimensions and measurements

PropertySelected valueRecorded rangeBasis
8,000 K5,000 K to 10,000 Kdefined reference

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Sources and method

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The source records and measurement method remain available for inspection.

Read the measurement and artwork methodology →

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