GS 3: Science & TechnologyPrelims

How do astronauts return from space and survive re-entry?, Pg9

Astronauts' perilous return: Mastering re-entry through heat shields, precise corridors, and parachute deployment for safe landing.

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Key Highlights:

  • Re-entry involves shedding immense orbital velocity against atmospheric resistance, converting kinetic energy into heat.
  • The blunt body theory deflects re-entry heat, preventing capsule melting.
  • A re-entry corridor is a precise atmospheric window for safe return, avoiding bouncing off or burning up.
  • Semi-ballistic bodies use an angle of attack to generate lift, enabling steering toward a landing zone.
  • A communication blackout occurs due to plasma interference, managed via relay satellites and high-frequency signals.
  • Parachutes are deployed to reduce velocity after aerobraking for a safe landing.
  • Gaganyaan's crew module (CM) will use a three-stage parachute system for a Bay of Bengal splashdown.
Gaganyaan

Gaganyaan

Detailed Insights:

  • Aerospace scientists initially thought atmospheric re-entry survival impossible due to extreme heat.
  • Over 98% of a re-entering capsule's energy dissipates as heat, shielded by ablative or thermal insulation systems.
  • Deorbit burn reduces velocity, causing gravity to overcome centrifugal force, initiating a downward trajectory.
  • Too shallow an entry angle causes the capsule to bounce off the atmosphere; too steep leads to lethal deceleration and heat.
  • Semi-ballistic bodies fly at an angle, creating lift for gliding and banking toward a targeted landing zone.
  • The plasma sheath during communication blackout blocks radio waves, disrupting communication until the capsule slows.
  • Aerobraking uses atmospheric drag to decelerate the capsule; parachutes further reduce velocity for a soft landing.
  • ISRO's Space Capsule Recovery Experiment (SRE) in 2007 and CARE in 2014 validated re-entry capabilities.
  • Gaganyaan's service module (SM) will be destroyed during re-entry; the CM will maneuver within the re-entry corridor.
  • The CM will modulate its lift vector via thruster firings to reach its Bay of Bengal landing site.

Key Concepts Involved:

  • Re-entry Corridor: The narrow atmospheric path a spacecraft must follow to safely return to Earth.
  • Semi-Ballistic Body: A vehicle that uses both aerodynamic lift and drag to control its descent.
  • Aerobraking: Using atmospheric drag to decelerate a spacecraft during re-entry.
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