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ISRO / NSIL · Operational · in · Launch Vehicle

LVM3 (GSLV Mk III)

India's heavy-lift rocket with a 100% success rate; two launches in 2025 (CMS-03 and AST SpaceMobile's BlueBird Block 2).

Verified 2026-09-24 · First flight 2014-12-18

Operator page

Systems cutaway

Systems
LVM3 (GSLV Mk III) — systems cutaway schematicPropulsion
2× S200 solid strap-on boosters (largest Indian solids); L110 liquid core stage (Vikas engines, UDMH/N2O4); C25 cryogenic upper stage (CE-20 LOX/LH2); 11,898 kN liftoff thrust.
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Structures
4 m core diameter; 43.5 m height; 5 m diameter payload fairing.
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LVM3 (GSLV Mk III)43.5 m
Propulsion↗

2× S200 solid strap-on boosters (largest Indian solids); L110 liquid core stage (Vikas engines, UDMH/N2O4); C25 cryogenic upper stage (CE-20 LOX/LH2); 11,898 kN liftoff thrust.

Structures↗

4 m core diameter; 43.5 m height; 5 m diameter payload fairing.

Specs & Metrics

Payload to LEO ↑ better
10,000 kg
Maximum payload mass deliverable to low Earth orbit (~200–400 km circular), in the vehicle's stated reference configuration.
Payload to GTO ↑ better
4,000 kg
Maximum payload mass deliverable to geostationary transfer orbit (~185 × 35,786 km), in the stated reference config.
Liftoff Thrust ↑ better
11898 kN
Total first-stage thrust at liftoff (sea-level), in kilonewtons, summing all active engines and solid strap-ons.
Liftoff Mass ↓ better
640 t
Total vehicle mass at liftoff including propellant, payload, and all stages, in metric tonnes.
Vehicle Height ↓ better
43.5 m
Full stack height at liftoff, in metres, including fairing or spacecraft.
Mission Success Rate ↑ better
100%
9 of 9 launches through LVM3-M6 (2025-12-24)
Percentage of launch attempts rated as full mission successes over the vehicle's complete flight history.
Launches in 2025 ↑ better
2
LVM3-M5/CMS-03 (Nov 2) and LVM3-M6/BlueBird Block 2 (Dec 24, 2025)
Total number of launch attempts conducted in calendar year 2025 (Jan 1 – Dec 31 UTC).

Subsystems

propulsion↗

2× S200 solid strap-on boosters (largest Indian solids); L110 liquid core stage (Vikas engines, UDMH/N2O4); C25 cryogenic upper stage (CE-20 LOX/LH2); 11,898 kN liftoff thrust.

structures↗

4 m core diameter; 43.5 m height; 5 m diameter payload fairing.