Payload LEO
6,000 kg
Payload GTO
2,500 kg
Assessment
Launch vehicle with a cryogenic upper stage for 2-tonne-class communications satellites (GTO); commercial sales discontinued in 2024, planned missions continue to fly (GSLV-F16 Jul 2025).
Technical data
Height49.1 m
Diameter3.4 m
Liftoff mass414.8 t
Liftoff thrust7,887 kN
Stages3
PropellantSolid + N2O4/UDMH + LOX/LH2
ReusabilityExpendable
First flight2010
Lead time–
Provider launch sites
Kulasekarapattinam SSLV Launch ComplexSDSC SHAR Third Launch Pad (TLP) – SriharikotaSatish Dhawan Space Centre (SDSC SHAR) – Sriharikota
Price
Price on requestPrices shown are the providers' official figures and are always non-binding – only the individual quote is binding.