/ Technology

Reusable by design, from the first sketch.

One family of AbyoKalaM engines, LOX/LNG propulsion and recoverable stages — engineered so the same hardware flies again, and the cost of reaching orbit falls with every flight.

50 kN
Test facility class
/ Products

Three vehicles, one engine family.

Reusable Suborbital Rocket — 01 vehicle render
01

Reusable Suborbital Rocket

200 Kg to LEO · 5 engines

Compact Reusable Launch Vehicle — 02 vehicle render
02

Compact Reusable Launch Vehicle

2.6 T to LEO, reusable · 9 engines

Medium Reusable Launch Vehicle — 03 vehicle render
03

Medium Reusable Launch Vehicle

15 T to LEO, reusable · 9 engines

/ End-to-end rocket infrastructure

Design, build, fire, fly — under one roof.

01

Design & simulation

Vehicle, engine and trajectory design modelled in-house before any metal is cut.

02

Manufacturing

Precision machining, composite layup and tank fabrication with Indian industry partners.

03

Engine test

Rocket Engine Test Facility — containerised, instrumented, up to 50 kN thrust.

04

Integration

Structures, avionics, propulsion and recovery married into a flight article.

05

Launch operations

Launch on demand — responsive campaigns on national timelines.

06

Recovery & reflight

Stages recovered, inspected and returned to the stand for the next mission.

Hardware in detail

Six systems that make a rocket fly twice.

AbyoKalaM engine
01

AbyoKalaM engine

Battleship-tested on Abyom's own stand.

LOX and LNG keep the propellant chain simple, cleaner to handle and easier to source at home — so test cadence is set by engineering, independent of logistics.

Regeneratively cooled
02

Regeneratively cooled

Engineered for reuse from the first sketch.

Propellant is routed through the chamber walls before it burns, pulling heat out of the structure. The same hardware can come back to the stand after each firing.

Pintle injection
03

Pintle injection

Pintle injector development, validated on the test stand.

A pintle injector trades complexity for control: stable combustion across a wide throttle range, with fewer parts to machine and fewer paths to validate.

Instrumented test bed
04

Instrumented test bed

Thrust, pressure and thermal telemetry on every fire.

Every hot fire is a data run. Thrust, chamber pressure and thermal maps are captured end to end, so each design change is judged on measurements rather than intuition.

Recovery system
05

Recovery system

Because a rocket that lands is a rocket that flies twice.

Staged deceleration and controlled descent bring the vehicle back intact — the difference between a launch programme and a manufacturing programme.

Modular payload bay
06

Modular payload bay

Payload-class configurable. Configurable per mission.

A common structural interface takes different dispensers and mounts, so customers integrate to one standard while each mission keeps its own layout.

/ Test facility

We fail on the ground,
so we don't in the sky.

Abyom's Rocket Engine Test Facility — a containerised platform for engines up to 50 kN thrust — has hosted Abyom's injector test campaign. Instrumented to the millisecond. Every valve, every weld and every line of flight code earns its place through hours of testing — then, and only then, flight.

50 kN
Test facility class