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Vikram-I engineering: Key specifications of Skyroot’s first orbital rocket
Vikram-I is a four-stage small-lift rocket using solid propulsion and a liquid final stage, capable of placing 290 kg payloads into low-Earth orbit.
Vikram-I is a four-stage small-lift launch vehicle designed to place satellites into low-Earth orbit. It uses solid propulsion in three stages and a liquid-based fourth stage for precise orbital insertion. The rocket supports payloads of up to 290 kg to a 500 km orbit and incorporates carbon-composite motor casings to reduce weight.