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| Attribute | GSLV Mk III (LVM3) 🇮🇳 India Trust: Agency-primaryⓘ Last verified Active · Last updated 2026-06-01Remove × | ||
|---|---|---|---|
| Company | ISRO | SpaceX | Avio |
| Country | 🇮🇳 India | 🇺🇸 USA | 🇪🇺 Europe |
| Status | Active | Active | In Development |
| Vehicle class | Heavy | Medium | Small |
| Propellant | Solid (S200 boosters) + UDMH/N₂O₄ (L110) + LH₂/LOX (C25) | RP-1 / LOX | Solid (P160C first stage) / LOX-methane (cryogenic upper stage) |
| Reusable | No | Yes | No |
| Stages | 3 | 2 | 3 |
| First flight | 2017 | 2010 | 2027 |
| Payload to LEO | 10,000 kgas of [1] | 22,800 kgas of [1]Reusable first stage (expended gives 22,800 kg; reused gives ~15,600 kg) ↑ Best | — |
| Payload to GTO | 4,000 kgas of [1] | 8,300 kgas of [1]Expendable configuration. Reusable GTO capacity ~5,500 kg. ↑ Best | — |
| Height | 43.43 mas of [1] | 70 mas of [1] ↑ Best | — |
| Liftoff mass | 643 tas of [1] ↑ Best | 549 tas of [1] | — |
| Success rate | 100%as of [2]10/10 missions since development flight 2014 (D1). Production flights since 2017. ↑ Best | 99.5%as of [2]~665/668 full successes (Falcon family incl. Falcon Heavy); 500th landing Sep 2025 | — |
| Total flights | 10as of [2] | ~668as of [2]Falcon family total (Falcon 9 + Falcon Heavy) per launch log; 75 in 2026 (74 F9 + 1 FH) as of Jun 25, 2026 ↑ Best | — |
| Cost / kg LEO | ~$4,500/kgas of [1]Estimated from OneWeb commercial contract ~$450M for 36 satellites (~5 tonne batch to GTO) | ~$2,720/kgas of [1]Based on $67M list price / 22,800 kg LEO (expendable) ↓ Cheapest | — |
| Summary | India's most powerful rocket. Launched Chandrayaan-3 (Moon lander) in Jul 2023 and OneWeb internet satellites commercially. Renamed LVM3 (Launch Vehicle Mark 3) in 2022. The CE-20 cryogenic engine was entirely ISRO-developed — previously India depended on Russian technology for the GSLV Mk II. | The world's most frequently flown orbital rocket. Block 5 first stages have landed over 280 times and reflown up to 23 times. Backbone of Starlink and commercial crewed launches. | The next evolution of ESA's Vega line: replaces the Zefiro-9 and AVUM+ stages with a single cryogenic LOX/methane upper stage powered by the new M10 engine, adding multi-orbit deployment flexibility. First flight is a stated target (2027), not yet flown. |
48 launch vehicles across 10 countries — active, retired, and in development — with primary-source citations from manufacturer user guides and agency press kits. Pure URL state: bookmark or share the link and the comparison reproduces exactly.