Chandrayaan-2
Chandrayaan-2, India’s second mission to the Moon, will have an Orbiter and Lander-Rover module. ISRO will have the prime responsibility for the Orbiter and Rover; Roskosmos, Russia will be responsible for Lander. Chandrayaan-2 will be launched on India’s Geosynchronous Satellite Launch Vehicle (GSLV-MkII) around 2012-13 timeframe. The science goals of the mission are to further improve the understanding of the origin and evolution of the Moon using instruments onboard Orbiter and in-situ analysis of lunar samples using Lander and Rover.
The following five payloads are selected for Orbiter.
1. Large Area Soft X-ray Spectrometer (CLASS) and Solar X-ray Monitor (XSM) for mapping the major elements present on the lunar surface.
2. L and S band Synthetic Aperture Radar (SAR)
for probing the first few tens of meters of lunar surface for the presence of different constituen including water ice. SAR is expected to provide further evidence confirming the presence of water ice below the shadowed regionsof the moon.
3. Imaging IR Spectrometer (IIRS) for mapping of lunar surface over a wide wavelength range for the study of minerals, water molecules and hydroxyl present.
4. Neutral Mass Spectrometer (ChACE-2) to carry out a detailed study of the lunar exosphere.
5. Terrain Mapping Camera-2 (TMC-2) for preparing a three-dimensional map essential for studying the lunar mineralogy and geology.
Following two scientific payloads selected for Indian Rover would carry out elemental analysis of the lunar surface near the landing site
1. Laser Induced Breakdown Spectroscope (LIBS).
2. Alpha Particle Induced X-ray Spectroscope (APIXS).
Chandrayaan-2, India’s second mission to the Moon, will have an Orbiter and Lander-Rover module. ISRO will have the prime responsibility for the Orbiter and Rover; Roskosmos, Russia will be responsible for Lander. Chandrayaan-2 will be launched on India’s Geosynchronous Satellite Launch Vehicle (GSLV-MkII) around 2012-13 timeframe. The science goals of the mission are to further improve the understanding of the origin and evolution of the Moon using instruments onboard Orbiter and in-situ analysis of lunar samples using Lander and Rover.
The following five payloads are selected for Orbiter.
1. Large Area Soft X-ray Spectrometer (CLASS) and Solar X-ray Monitor (XSM) for mapping the major elements present on the lunar surface.
2. L and S band Synthetic Aperture Radar (SAR)
for probing the first few tens of meters of lunar surface for the presence of different constituen including water ice. SAR is expected to provide further evidence confirming the presence of water ice below the shadowed regionsof the moon.3. Imaging IR Spectrometer (IIRS) for mapping of lunar surface over a wide wavelength range for the study of minerals, water molecules and hydroxyl present.
4. Neutral Mass Spectrometer (ChACE-2) to carry out a detailed study of the lunar exosphere.
5. Terrain Mapping Camera-2 (TMC-2) for preparing a three-dimensional map essential for studying the lunar mineralogy and geology.
Following two scientific payloads selected for Indian Rover would carry out elemental analysis of the lunar surface near the landing site
1. Laser Induced Breakdown Spectroscope (LIBS).
2. Alpha Particle Induced X-ray Spectroscope (APIXS).