Payload LEO
500 kg
Payload SSO
300 kg
Assessment
Small launch vehicle for small satellites (500 kg to 500-km LEO, 300 kg to SSO); operational since the successful SSLV-D3 flight (Aug 2024) and marketed by NSIL.
Technical data
Height34 m
Diameter2 m
Liftoff mass120 t
Liftoff thrust2,496 kN
Stages3
PropellantSolid (HTPB)
ReusabilityExpendable
First flight2022
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.