It's not air friction that heats space shuttle?

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SUMMARY

The heating of fast-moving objects, such as the Space Shuttle, during atmospheric entry is primarily due to highly compressed air at the leading edges, rather than air friction. At an altitude of approximately 33,000 feet (11,000 km), the static pressure is about 23 kPa, with a temperature of -56.5°C. When the Shuttle travels at a speed of 20,000 km/h (5,555 m/s), the calculated stagnation pressure at the nose is approximately 5.6 MPa (56 bar or 812 PSI). This information clarifies common misconceptions about the thermal dynamics of atmospheric re-entry.

PREREQUISITES
  • Understanding of fluid dynamics principles
  • Familiarity with atmospheric pressure and temperature concepts
  • Knowledge of the Space Shuttle's operational parameters
  • Basic calculations involving pressure and velocity
NEXT STEPS
  • Research the effects of stagnation pressure on spacecraft design
  • Explore the principles of aerodynamics related to atmospheric entry
  • Learn about the thermal protection systems used in spacecraft
  • Investigate the physics of meteoroids entering Earth's atmosphere
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Aerospace engineers, physics students, and anyone interested in the dynamics of atmospheric re-entry and spacecraft design.

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I read an article in a science mag. awhile back entitled "The ten misconceptions NASA tour guides hear". They said that air friction is not responsible for the heating of fast moving objects through the atmosphere, but highly compressed air at the leading edges. Now that I am enlightened, could anyone tell me the PSI that the shuttle sees on its nose area? Also the temp? This may be a tough one, but how about the PSI and temp of a meteor entering our atmosphere? Thanks Guys!
 
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ok, let's say the stagnation pressure is the sum of the dynamic and static pressure at the nose of the shuttle when it's in the tropopause (11000km around 33000ft altitude). The static pressure at this altitude is about 23kPa, the temperature is about -56.5°C and the density of the air is around 0.36kg/m³.

So dynamic pressure is 1/2*density*v²
let's assume the shuttle is doing about 20000km/h (5555m/s) at this point, the stagnation pressure would be 1/2*0.36*5555² + 23000 = 5577444.5Pa = 5.6MPa = 56bar! (812Psi)

this is a very rough approximation, but use it as you like.
 

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