Chandrayan Live Telicast
Chandrayaan 3 Live Updates : Vikram Lander scheduled to make soft landing at 6.04pm tomorrow Ahead of the historic landing scheduled for tomorrow at 6.04 pm , the Indian Space Research Organisation ( ISRO ) announced on Monday that they will organise a live telecast of the landing process , which will begin at 5.20 pm on the same day . The link for the livestreaming has also been shared and is available on ISRO's official website . New Delhi , Aug 20 ( ANI ) : Indian Space Research Organisation ( ISRO ) announces the landing of Chandrayaan - 3 on the moon on August 23 2023 , on Sunday . ( ANI Photo ) New Delhi , Aug 20 ( ANI ) : Indian Space Research Organisation ( ISRO ) announces the landing of Chandrayaan - 3 on the moon on August 23 2023 , on Sunday
Lander payloads: Chandra’s Surface Thermophysical Experiment (ChaSTE) to measure the thermal conductivity and temperature; Instrument for Lunar Seismic Activity (ILSA) for measuring the seismicity around the landing site; Langmuir Probe (LP) to estimate the plasma density and its variations. A passive Laser Retroreflector Array from NASA is accommodated for lunar laser ranging studies.
Integrated Cold Test - For the demonstration of Integrated Sensors & Navigation performance test using helicopter as test platform
Integrated Hot test – For the demonstration of closed loop performance test with sensors, actuators and NGC using Tower crane as test platform
Lander Leg mechanism performance test on a lunar simulant test bed simulating different touch down conditions.
Chandrayaan-3 consists of an indigenous Lander module (LM), Propulsion module (PM) and a Rover with an objective of developing and demonstrating new technologies required for Inter planetary missions. 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 Lander and the Rover have scientific payloads to carry out experiments on the lunar surface.
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The main function of PM is to carry the LM from launch vehicle injection till final lunar 100 km circular polar orbit and separate the LM from PM. Apart from this, the Propulsion Module also has one scientific payload as a value addition which will be operated post separation of Lander Module. The launcher identified for Chandrayaan-3 is LVM3 M4 which will place the integrated module in an Elliptic Parking Orbit (EPO) of size ~170 x 36500 km.
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