LVM-3 | Chandrayaan-4 Second Launch
To Be Determined
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Chandrayaan-4 is a planned lunar sample-return mission of Indian Space Research Organisation (ISRO) and will be the fourth mission of its Chandrayaan programme. The mission consist of five modules, namely the DM (Descender Module), AM (Ascender Module), TM (Transfer Module), RM (Re-entry Module) and PM (Propulsion Module). The planned mission life is 1 lunar day and the landing site will be near the Lunar South Pole. The second launch will lift the TM (Transfer Module), RM (Re-entry Module) and PM (Propulsion Module) to orbit.
Added launch.
The Launch Vehicle Mark-3 (LVM-3), previously called Geosynchronous Satellite Launch Vehicle Mark III (GSLV Mk III), is a three-stage medium-lift launch vehicle developed by the Indian Space Research Organisation (ISRO). It is designed to launch satellites into geostationary orbit, and is intended as a launch vehicle for crewed missions under the Indian Human Spaceflight Programme.
The Indian Space Research Organisation (ISRO) is the space agency of the Government of India headquartered in the city of Bangalore. Its vision is to "harness space technology for national development while pursuing space science research and planetary exploration."
INFO WIKI
HELSINKI — India’s Chandrayaan-4 lunar sample return mission will target a landing between 85 and 90 degrees latitude in the southern hemisphere of the moon, and follow up with a […]
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