The Gaganyaan crew module, designed with a sphere-cone re-entry configuration, will carry Indian astronauts into orbit and safely return them via sea splashdown. The article details the engineering trade-offs between aerodynamic stability, dynamic instability, and hydrodynamic mono-stability critical for the crew module's survival during descent. Key design features include a detached shockwave for heat management and a redundant joint separation mechanism from the service module.
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- ›Mission Type: India's maiden crewed space mission
- ›Crew Module Configuration: Sphere-cone
- ›Target this Mission: Gaganyaan - India's maiden crewed space mission
- ›Target this Design: Sphere-cone configuration for crew module
- ›Target this Institution: ISRO (Indian Space Research Organisation)
- ›Target this Rocket: HLVM-3 (Human-rated Launch Vehicle Mark 3)
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