INSUBCONTINENT EXCLUSIVE:
12-19 window and will make a second attempt at soft-landing on the south pole side of Moon, which, if successful, will put India in the
elite club of three nations (US, Russia and China) with moon-landing capability
If the spacecraft is launched successfully next week, it will travel towards the Moon for over a month covering a distance of about 3.84
lakh km and will attempt a safe landing on the south pole side around August 23.Chandrayaan-3 is a follow-on mission to Chandrayaan-2
Unlike its predecessor, which carried an orbiter along with Vikram lander and Pragyan rover, Chandrayaan-3 is a composite of three modules:
propulsion, lander and rover
The total weight of the spacecraft is 3,900 kg, which is a tad lower than the total carrying capacity of LVM3
The propulsion module weighs 2,148 kg and the lander 1,752 kg, including the rover
Incidentally, the Chandrayaan-2 payload weighed about 3.8 tonnes with the orbiter weighing 2,379 kg.After its failed landing attempt on
September 6, 2019, Isro has since carried out several changes on the lander for Chandrayaan-3 mission
This time Vikram will have stronger legs than in its previous version to enable withstanding landing at greater velocities than earlier,
while Isro has also made several other changes learning from the failures of the Chandrayaan-2 mission
The propulsion module has spectro-polarimetry of habitable planet earth (SHAPE) payload to study the spectral and polari metric measurements
of Earth from the lunar orbit
Lunar Seismic Activity (ILSA) for measuring the seismicity around the landing site; Langmuir Probe (LP) to estimate the plasma density and
its variations, and a passive Laser Retroreflector Array from Nasa is accommodated for lunar laser ranging studies.The rover payloads are
Alpha Particle X-ray Spectrometer and Laser Induced Breakdown Spectroscope for deriving the elemental composition in the vicinity of the
The main function of the propulsion module is to carry the lander module from launch vehicle injection till the final lunar 100 km circular
polar orbit and separate the lander from the propulsion
Apart from this, the propulsion module also has one scientific payload as a value addition that will be operated post separation of the
