Sriharikota: The Indian Space Research Organisation (ISRO) on Thursday announced that its lunar mission Chandrayaan-3 will be launched on July 14 from the space port at Sriharikota in Andhra Pradesh. ISRO’s new heavy lift launch vehicle LVM-3 will carry out the Moon mission. ISRO to attempt soft-landing on Moon on August 23 or August 24 said ISRO’s Chairman Somanath S.
“Announcing the launch of Chandrayaan-3: LVM3-M4/Chandrayaan-3 Mission: The launch is now scheduled for July 14, 2023, at 2:35 pm IST from SDSC (Satish Dhawan Space Centre), Sriharikota,” ISRO tweeted. The Chandrayaan-3 mission carries scientific instruments to study the thermophysical properties of the lunar regolith, lunar seismicity, lunar surface plasma environment and elemental composition in the vicinity of the landing site.
In March this year, the Chandrayaan-3 spacecraft successfully completed the essential tests that validated its capability to withstand the harsh vibration and acoustic environment that the spacecraft would encounter during its launch. These tests were particularly challenging, considering the fact that the Chandrayaan-3 spacecraft, which will be launched by LVM3 (Launch Vehicle Mark-III) (earlier referred to as GSLV Mk III), is a composite of three modules — propulsion, lander and rover.
The propulsion module, which has Spectro-polarimetry of Habitable Planet Earth (SHAPE) payload to study the spectral and polarimetric measurements of Earth from the lunar orbit, will carry the lander and rover configuration till 100 km of the lunar orbit. The lander payloads are: ‘Chandra’s Surface Thermophysical Experiment’ to measure the thermal conductivity and temperature; ‘Instrument for Lunar Seismic Activity’ for measuring the seismicity around the landing site; and ‘Langmuir Probe’ to estimate the plasma density and its variations.
A passive Laser Retroreflector Array from US space agency National Aeronautics and Space Administration (NASA) is also accommodated for lunar laser ranging studies. The rover payloads are: ‘Alpha Particle X-ray Spectrometer’ and ‘Laser Induced Breakdown Spectroscopy’ for deriving the elemental composition in the vicinity of the landing site. The lander will have the capability to soft land at a specified lunar site and deploy the rover which will carry out in-situ chemical analysis of the lunar surface during the course of its mobility.
The main function of the propulsion module is to carry the lander module from launch vehicle injection till final lunar 100 km circular polar orbit and separate it. Apart from this, the propulsion module also has one scientific payload as a value addition, which will be operated post separation of the lander module.
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