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GSLV Mk.3 (2) (LVM-3 (2))
 GSLV Mk.3 (2) (GSat 29) [ISRO] |
LVM-3 or GSLV Mk.3 is an Indian launch vehicle capable of launching a four ton satellite into geosynchronous transfer orbit. LVM-3 is a three-stage vehicle with a 110 ton core liquid propellant stage (L-110) and a strap-on stage with two solid propellant motors, each with 200 tons propellant (S-200). The upper stage will be cryogenic fueled with a propellant loading of 25 tons (C-25). LVM-3 will have a lift-off weight of about 629 tons and will be 42.4 m tall. The payload fairing has a diameter of 5 m and a payload volume of 100 cubic meters.
For the suborbital first flight, X-1, the second stage was inert without an engine. The data from this test flight resulted in a number of changes - a different ogive shape of the payload fairing and slanted nosecones for the boosters.
After the first orbital flight, an enlarged cryogenic stage was introduced.
| Version | Strap-On | Stage 1 | Stage 2 |
|---|---|---|---|
| GSLV Mk.3 (2) (LVM-3 (2)) | 2 × S-200 | L-110 / 2 × HTVE | C-25 / CE20 |
| Performance (kg) | LEO | LPEO | SSO | GTO | GEO | MolO | IP |
|---|---|---|---|---|---|---|---|
| GSLV Mk.3 (2) (LVM-3 (2)) |
No: TypeNo: Type Serial Date LS Payload
3 1 GSLV Mk.3 (2) D2 14.11.2018 Sr SLP GSat 29 4 2 LVM3 (2) M1 22.07.2019 Sr SLP Chandrayaan 2 / Vikram 5 3 LVM3 (2) M2 22.10.2022 Sr SLP OneWeb L14-1, ..., L14-36 6 4 LVM3 (2) M3 26.03.2023 Sr SLP OneWeb L18-1, ..., L18-36 7 5 LVM3 (2) M4 14.07.2023 Sr SLP Chandrayaan 3 / Vikram 2 Planned: x x LVM3 (2) Mx xx.xx.202x Sr SLP Gaganyaan 1 x x LVM3 (2) Mx xx.xx.202x Sr SLP Gaganyaan 2 x x GSLV Mk.3 (2) Mx xx.xx.202x Sr SLP GSat 20 (CMS 03) x x GSLV Mk.3 (2) Mx xx.xx.202x Sr SLP GSat 22 ? Launch sites: Sr = Satish Dhawan Space Center (Sriharikota Space Center), Sriharikota, Andhra Pradesh, India
