Small Satellite Launch Vehicle (or SSLV) is a launch vehicle being developed by the Indian Space Research Organisation (ISRO) with payload capacity of 500 kg to Low Earth orbit or 300 kg to Sun synchronous orbit for launching small satellites, with the capability to support multiple orbital drop-offs.
Specifications
- Thrust
- —
- Height
- 34 m
- Diameter
- 2 m
- Launch mass
- 120 t
- Stages
- 4
- Launch cost
- —
- LEO capacity
- 500 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- 300 kg
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
3
Launches with a definitive outcome
Success rate
66.7%
2 of 3
Current success streak
2
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- SSLV | EOS-08/Microsat-2C — Success
- SSLV | EOS-7 & rideshare (Demo 2) — Success
- SSLV | EOS-02 (Microsat-2A) (Demo 1) — Failure