Live
- 3rd Test: Day one’s play at the Gabba called off due to persistent rain
- National Energy Conservation Day: Switch to Energy-Efficient Devices
- Rekha gets emotional as she shares a heartfelt moment with Big B's grandson Agastya Nanda
- Senior Cong leader EVKS Elangovan passes away in Chennai
- CID's Counter Intelligence raids multiple places in J&K’s Anantnag, Kulgam districts
- India's growth on resilient trajectory, equity markets in consolidation phase
- KJo on 23 years of ‘Kabhi Khushi Kabhie Gham’: One of those pinch me moments
- WPL 2025 auction: Nandini, Kamalini set to be most sought-after names
- MP CM to inaugurate Sarsi resort in Shahdol, 200-bed hospital in Mauganj today
- TGPSC makes arrangements for Group-2 exams to be held tomorrow
Unique experiment: Chandrayaan-3 propulsion module moved to orbit Earth
Bengaluru: The Propulsion Module (PM) of Chandrayaan-3 has been moved from an orbit around the Moon to an orbit around Earth, ISRO has said, terming...
Bengaluru: The Propulsion Module (PM) of Chandrayaan-3 has been moved from an orbit around the Moon to an orbit around Earth, ISRO has said, terming the operation a unique experiment. The primary objective of the Chandrayaan-3 mission was to demonstrate a soft landing near the lunar south polar region and perform experiments using the instruments on the 'Vikram' lander and the 'Pragyan' rover. The spacecraft was launched on July 14, 2023, on board the LVM3-M4 vehicle from the Satish Dhawan Space Centre (SDSC-SHAR).
On August 23, the Vikram lander made its historic touchdown on the Moon and subsequently, the Pragyan rover was deployed. The scientific instruments in the lander and rover were operated continuously for one lunar day as per the defined mission life. "The mission objectives of Chandrayaan-3 have been completely met," the Indian Space Research Organisation (ISRO) said in a statement.
For the Propulsion Module, the main objective was to ferry the lander module from the Geostationary Transfer Orbit (GTO) to the final lunar polar circular orbit and separate the lander, it said. After the separation, the Spectro-polarimetry of HAbitable Planet Earth (SHAPE) payload in the PM was also operated, the space agency said. The initial plan was to operate this payload for about three months during the mission life of the PM. The precise orbit injection by LVM3 and optimal earth or lunar burn manoeuvres resulted in the availability of over 100 kg of fuel in the PM after over one month of operations in the lunar orbit, it added.
ISRO said that it was decided to use the available fuel in the PM to derive additional information for future lunar missions and demonstrate the mission operation strategies for a sample return mission. To continue the SHAPE payload for earth observation, it was decided to re-orbit the PM to a suitable earth orbit. This mission plan was worked out considering collision avoidance such as preventing the PM from crashing onto the Moon’s surface or entering into the Earth’s Geosynchronous Equatorial Orbit (GEO) belt at 36,000 km and orbits below that, the statement said. Considering the estimated fuel availability and the safety of the GEO spacecraft, the optimal earth return trajectory was designed for October 2023.
