ABOUT VIKRAM-I
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.
PAYLOAD CAPACITY
350 kg
TO LEO
772 lbs
LIFTOFF THRUST
1,200
KILONEWTONS
269,771
POUNDS-FORCE
~1,609
HORSEPOWER
FLIGHT HISTORY
⚙ RELATED ENGINES