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