Skyroot Aerospace

Vikram-I

Vikram-I
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Overview

/01

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.

Manufacturer

Skyroot Aerospace

Variant

N/A

Alias

N/A

Maiden Flight

N/A

Technical Specifications

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20 m

Length

1.7 m

Diameter

—

Launch Mass

1200 kN

Liftoff Thrust

350 kg

LEO Capacity

—

GTO Capacity

Launch Record

/03
0

Total Launches

0

Successful

0

Failed

—

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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