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Vikram-1

Operational

Skyroot Aerospace first orbital launch carrying multiple commercial microsatellites for international clients. 450-Km, LEO

Vehicle Specifications

Height

—

Diameter

—

Lift-off Mass

—

Booster Stages

—

Payload (LEO)

350.0 kg

Payload (GTO)

—

Modular Booster Stages

S1

Stage 1

Solid Booster

Provides massive thrust at lift-off utilizing advanced HTPB solid propellants.

S2

Stage 2

Liquid Core

High-efficiency liquid engine powering the vehicle through atmospheric climb.

S3

Stage 3

Cryogenic Stage

Highly advanced cryogenic upper stage for precise orbital injection in GTO.

Vikram-1

Launch Roster Performance

100%Success
First Flight LaunchUnknown
Total Mission Runs—
Successful Missions—
Failed Missions0

Mission Status

This launcher configuration is categorized under Active Launch Roster Fleet. It remains one of the fundamental benchmarks of ISRO's satellite deployment program.