Vikram-I Vehicle Overview
A complete overview of the Vikram-I launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
Vikram-I
Family
Vikram
Manufacturer
First Launch
Not Yet Launched
Successful Launches
0
Failed Launches
0
Rocket Info
Status
Active
Stages
4
Length
20 m
Diameter
1.7 m
Thrust
1,200 kN
Reusability
Not Reusable
Payload Info
LEO Capacity
350 kg
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.
Launch Sites used by Vikram-I
Satish Dhawan Space Centre
India's primary spaceport, launching lunar, Mars missions, and satellites, located in Andhra Pradesh.
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