SUMMARY
The space shuttle's re-entry burn lasts approximately 30 minutes, although the intense heating phase, where temperatures reach around 1500°C, is significantly shorter. The re-entry process includes a period of ionization blackout lasting about 12 minutes, during which radio communication is disrupted. The discussion highlights the confusion regarding the duration of the burn and clarifies that the shuttle does not experience a complete ionization blackout. Additional questions regarding the altitude during the burn phase were raised, indicating a need for precise data on vertical height.
PREREQUISITES
- Understanding of space shuttle re-entry dynamics
- Knowledge of thermal protection systems used in aerospace
- Familiarity with ionization effects during atmospheric re-entry
- Basic principles of aerodynamics and atmospheric physics
NEXT STEPS
- Research the thermal protection materials used in the Space Shuttle, such as Reinforced Carbon-Carbon (RCC)
- Learn about the physics of ionization blackout and its effects on spacecraft communication
- Investigate the specific altitude profiles of the Space Shuttle during re-entry
- Explore the differences in re-entry profiles among various spacecraft, including the SpaceX Dragon
USEFUL FOR
Aerospace engineers, space enthusiasts, and students studying aerospace dynamics will benefit from this discussion, particularly those interested in the re-entry processes of the Space Shuttle and related thermal protection technologies.