LVM-3 | Chandrayaan-4 Second Launch

Chandrayaan-4 Second Launch

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.

Launch Vehicle Mark-3 (GSLV Mk III)

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.

Length

43.4 m

Diameter

4 m

Launch Mass

629 t

LEO Capacity

10,000 kg

GTO Capacity

5,000 kg

Maiden Flight

2014