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Vikram-I
Skyroot Aerospace
Details
Height
20 m
Diameter
1.7 m
GTO
Unknown
LEO
350 kg
Thrust at Liftoff
1,200 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
July 18, 2026
Statistics
Pro
Pro upgrade required for advanced features
Description
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.
Agency
Skyroot Aerospace
Skyroot
Links
Website
skyroot.in
Wikipedia
en.wikipedia.org