With reference to the design of the Gaganyaan crew module, consider the following statements:
- The crew module uses a pure spherical shape, similar to the Soviet Vostok module, to maximise internal volume and minimise structural mass.
- A blunt, rounded base in the module's design generates a detached shockwave ahead of the spacecraft, deflecting frictional heat away from its skin during re-entry.
- Because of its asymmetric shape, the crew module has two stable aerodynamic positions and two stable hydrodynamic positions, requiring control thrusters and a gas-based uprighting system to manage instability.
Which of the statements given above is/are correct?
Tests the ability to correctly attribute a specific engineering design choice to the right spacecraft, rather than confusing it with a historically related but distinct design.
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