What is the primary function of the Crew Escape System (CES) on ISRO's Human Rated LVM3 (HLVM3) rocket?
ATo guide the crew module into its designated Low Earth Orbit.
BTo eject the crew module to safety during launch emergencies.
CTo assist in docking the crew module with a space station.
DTo provide thermal shielding during re-entry into Earth's atmosphere.
