4-stage orbital launch vehicle developed by Indian private company Skyroot Aerospace, with capability of up to 350 kg to Low Earth Orbit. The first 3 stages are powered by solid fuel rocket motors, topped by a hypergolic fuel upper stage.
Specifications
- Thrust
- 1,200 kN
- Height
- 20 m
- Diameter
- 1.7 m
- Launch mass
- —
- Stages
- 4
- Launch cost
- —
- LEO capacity
- 350 kg
- GTO capacity
- —
- GEO capacity
- —
- SSO capacity
- 260 kg
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
1
Launches with a definitive outcome
Success rate
100%
1 of 1
Current success streak
1
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
- Vikram-I | Demo Flight — Success