Payload LEO
100 kg
Assessment
Customisable two stage small satellite launcher with 3D printed semi-cryogenic Agnilet engines on the first stage and an Agnite engine on the second stage. The first orbital mission, scheduled for a launch window in the first quarter of 2027, carries up to 100 kg to LEO, and the second mission, planned for the second quarter of 2027, up to 300 kg. Launches take place from Agnikul Launchpad-01 at Sriharikota.
Technical data
Stages2
PropellantSemi-cryogenic, LOX oxidiser
Lead time–
Price
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