Vikram-I
Vikram familySkyroot AerospaceActive
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
- Stages
- 4
- LEO capacity
- 350 kg
- SSO capacity
- 260 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
1flightwith a definitive outcome
100%success rate1 of 1
1success streakcurrent
Counted from padside's own launch record, the same basis as the stats page.