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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

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

Scale illustration of Space Shuttle re-entry plasma, showing the recorded representative plasma temperature.
Recorded representative plasma temperature: 8,000 K.

A little perspective

Space Shuttle re-entry plasma vs Sun: temperature comparison

The plasma temperature of Space Shuttle re-entry plasma is 2,228 K higher than the surface temperature of the Sun.

Scale
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.

8,000 KRepresentative plasma temperature
0 K · absolute zero
Sun

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

5,772 KSurface temperature
0 K · absolute zero
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

Representative plasma temperature: 8,000 K; defined reference; range 5,000 K–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.

Defined examples — our methodology

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

Sun

Surface temperature: 5,772 K; approximate.

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.

Use the visual comparison to explore its scale, then check the measurements and sources.

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Why this measurement?

Why we use 8,000 K

We compare the plasma temperature of Space Shuttle re-entry plasma. This is an illustrative comparison value, not a claim that every example is the same. 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 picture identifies the subject; the diagram compares the recorded values. How calibrated comparisons work →

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Recorded properties

Dimensions and measurements

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

Around this scale

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Sources and method

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The source records and measurement method remain available for inspection.

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