Lander includes Instrument for Lunar Seismic Activity (ILSA) Seismometer. It is used
The launcher identified for Chandrayaan-3 is ____________
The Vertical velocity during the lander touchdown will be
Chandra’s Surface Thermo physical Experiment (ChaSTE). The objective is
LASER Induced Breakdown Spectroscope (LIBS). The objective is to
The total mass of Chandrayaan-3 is
The Mission Life of Lander & Rover are
The mission objectives of Chandrayaan-3
The Spectro-polarimetry of HAbitable Planet Earth (SHAPE) is the __________ module payload
Instrument for Lunar Seismic Activity (ILSA) is a ____________ payload