VIKRAM-I
EXPENDABLE 4-STAGE LAUNCH VEHICLE
INACTIVE
Technical Overview
Length
height
20
m
Diameter
radio_button_unchecked
1.7
m
Payload to LEO
rocket
350
kg
Payload to SSO
satellite_alt
260
kg
Engine Details
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.
Reusability
Expendable
Stages
4
Liftoff Thrust
1,200 kN
Flight History
*Current Launch Library totals
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Total Launches
0
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Tracked launch count
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Successful Launches
0
verified
Completed launches
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Failed Launches
0
schedule
1 pending