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Micro turbojet · 300 N-class

AIR300

Next-generation, mission-adaptable propulsion.

Range

Deeper strike ability

Low fuel burn
High thrust-to-weight
Lightweight build
Architecture

Inside AIR300

The 3D-printed combustor includes the ignition system. Printing parts as one piece means fewer parts to make and assemble.

01 INLET & START02 COMPRESSOR03 SHAFT04 AM COMBUSTOR05 TURBINE06 CASING & NOZZLE
  1. 01Inlet & start
  2. 02Compressor
  3. 03Shaft
  4. 04AM combustor
  5. 05Turbine
  6. 06Casing & nozzle
Simplified schematic · not to scale
Mission value

Why AIR300

Aira develops ECU software, wiring and instrumentation alongside the propulsion hardware, with design and test capability under one roof in Bicester.

01

Adapted to your mission

Configurable ECU software, sensing and interfaces, from long-endurance UAVs to target systems.

02

Rapid start-up ignition

Integrated ignition and ECU control for quick, dependable starts.

03

Direct UK engineering support

Work directly with the engineers in Bicester on controls, wiring and installation.

Datasheet

Full specification on request

Contact

Tell us what you need to fly.

Tell us about your engine requirement or engineering project and one of our engineers will get back to you.

Facility61 Wedgwood Road, Bicester
Oxfordshire OX26 4UL
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