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Chandrayaan-3 Propulsion Module moved from Moon orbit to Earth’s orbit, ISRO says 'returns to home'

Chandrayaan-3 Propulsion Module: It was decided to use the available fuel in the Propulsion Module to derive additional information for future lunar missions and demonstrate the mission operation strategies for a sample return mission, ISRO said.

Edited By: Raju Kumar @rajudelhi123 Bengaluru Updated on: December 05, 2023 9:02 IST
Propulsion Module (PM) of Chandrayaan-3
Image Source : ISRO Propulsion Module (PM) of Chandrayaan-3

Chandrayaan-3 Propulsion Module: The Indian Space Research Organization (ISRO) said on the Vikram Lander, the Propulsion Module (PM) of Chandrayaan-3 was moved from an orbit around the Moon to an orbit around the Earth.

"In another unique experiment, like the hop experiment on the Vikram Lander, the Propulsion Module (PM) of Chandrayaan-3 was moved from an orbit around Moon to an orbit around Earth," ISRO said in a statement released on December 4.

The primary objective of the Chandrayaan-3 mission was to demonstrate soft landing near to lunar south polar region and perform experiments using the instruments on Vikram and Pragyaan. The spacecraft was launched on July 14, 2023 on-board LVM3-M4 vehicle from SDSC, SHAR. On August 23rd Vikram Lander made its historic touchdown on Moon and subsequently Pragyaan rover was deployed.

"The scientific instruments in Lander and Rover were operated continuously for 1 lunar day as per the defined mission life. The mission objectives of Chandrayaan-3 have been completely met. With regard to the Propulsion Module, the main objective was to ferry the Lander module from GTO to the final lunar polar circular orbit and separate the Lander. Subsequent to separation, Spectro-polarimetry of HAbitable Planet Earth (SHAPE) payload in the PM was also operated. The initial plan was to operate this payload for about three months during the mission life of PM," it read.

The precise orbit injection by LVM3 and optimal earth/lunar burn manoeuvre resulted in the availability of over 100 kg of fuel in the PM after over one month of operations in the lunar orbit, the statement said.

"In order to continue 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 the collision avoidance such as preventing the PM from crashing onto the Moon’s surface or entering into the Earth’s GEO belt at 36000 km and orbits below that. Considering the estimated fuel availability and the safety to GEO spacecrafts, the optimal Earth return trajectory was designed for October 2023 month," it read.

The first manoeuvre was performed on October 9, 2023 to raise apolune altitude to 5112 km from 150 km thus, increasing the period of orbit from 2.1 hours to 7.2 hours.

"Later, considering the estimate of available propellant, the second manoeuvre plan was revised to target an Earth orbit of 1.8 lakhs x 3.8 lakhs km. The Trans-Earthinjection (TEI)maneuver was performed on October 13, 2023. In thepost-TEI maneuver realized orbit, the propulsion module made four Moon fly-bys before departing Moon SOI on November 10. Currently, propulsion module is orbiting Earth and crossed its first perigee on November 22nd with an altitude of 1.54 lakhs km. The orbit period is nearly 13 days with 27 deg inclination. The perigee and apogee altitude vary during its trajectory and the predicted minimum perigee altitude is 1.15 lakhs km. Hence as per current orbit prediction, there is no threat of close approach with any operational Earth orbiting satellites," it read.

As per the plan, the SHAPE payload is being operated whenever Earth is in its field of view, ISRO said.

Also, a special operation of the SHAPE payload was carried out on October 28, 2023, during a Solar Eclipse. The Shape payload operations will continue further.

UR Rao Satellite Centre/ISRO’s flight dynamics team has developed an analysis tool from first principles for this operation which is being validated through the return maneuvers carried out for the Chandrayaan-3 PM. The following are the main outcomes from the return manoeuvres carried out on CH3 PM related to future missions:

Planning and execution of trajectory and manoeuvres to return from the Moon to Earth. Development of a software module to plan such a manoeuvre and its preliminary validation. Planning and execution of a gravity-assisted flyby across a planets/ celestial body. Avoiding uncontrolled crashing of the PM on the Moon’s surface at the end of life of PM thus meeting the requirements of no debris creation.

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