Why Chandrayaan-3 is called Vikram lander?
Lander and Rover: Similar to Chandrayaan-2, Chandrayaan-3 was expected to consist of a lander and a rover. The lander would be designed to safely descend to the lunar surface and deploy the rover onto the Moon.
Mission Objective: The primary objective of Chandrayaan-3 would be to achieve a successful soft landing on the Moon. This would involve developing a robust landing system to ensure a controlled descent and landing.
Site Selection: The specific landing site for Chandrayaan-3 had not been finalized as of my last update. ISRO would likely choose a different landing site on the Moon's surface, possibly avoiding the challenges that led to the unsuccessful landing of the Vikram lander during Chandrayaan-2.
Scientific Goals: Like its predecessors, Chandrayaan-3 would also have scientific objectives, including studying the Moon's surface, its mineral composition, lunar geology, and potentially searching for water ice in permanently shadowed regions.
Launch Vehicle: Chandrayaan-3 would be launched into space using a suitable launch vehicle, likely the GSLV Mk III (Geosynchronous Satellite Launch Vehicle Mark III), which is capable of carrying the necessary payload to the Moon.
Orbiter: An orbiter would be responsible for circling the Moon and conducting various scientific observations from lunar orbit. It could study the lunar surface, map its composition, and analyze the Moon's exosphere and other phenomena.
Lander: The lander component would be designed to make a soft landing on the lunar surface. It would carry scientific instruments to analyze the local environment, gather data about the Moon's geology, and potentially conduct experiments related to the Moon's surface and subsurface.
Rover: A rover could be included to explore the lunar surface more extensively. It could travel across the terrain, collect samples, and perform scientific experiments. A rover would provide a close-up view of the Moon's surface and contribute to our understanding of its geological history.
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