OverviewMost electric aircraft today are built on compromises. They start with existing airframes and retrofit them with batteries — resulting in limited capacity, short endurance, and mission times that barely exceed 30–45 minutes when reserves are included. The MA-2 is a clean-sheet design developed specifically around its electric powertrain, with optimized aerodynamics and an integrated battery system to deliver practical mission endurance for operators and flight schools.
Key features- >220 NM / >400 km Range — Extended range for point-to-point missions within the class.
- 2–2.5 Hours Endurance — Real mission flight time accounting for reserves.
- 170 kWh Battery Capacity — Aircraft-integrated battery system sized for climb performance and sustained cruise.
- Clean-Sheet Design — Airframe and systems engineered from the outset for electric propulsion.
- Lightweight Composite-Metal Structure — Hybrid construction balancing weight and structural loads.
- Maximum Aerodynamic Efficiency — Low-drag geometry optimized for electric cruise profiles.
- 12 m Wingspan — High-aspect wing to support battery mass efficiently.
- 120 kt / 220 km/h Cruise Speed — Operational cruise suitable for regional missions.
- Swiss-made Engineering — Precision design and manufacturing standards.
- Sporty Handling — Responsive and balanced control characteristics.
- Emission-Free & Quiet Operation — Zero in-flight emissions and reduced acoustic footprint.
DatasheetDatasheet of the MA-2 is available (MA-2 datasheet referenced on the page).
Technical specifications- Model: MA-2 (referenced datasheet)
- Range: >220 NM / >400 km
- Endurance: 2–2.5 hours (real mission flight time)
- Battery capacity: 170 kWh (aircraft-integrated battery system)
- Design: Clean-sheet design optimized for electric propulsion
- Structure: Lightweight composite-metal hybrid
- Wingspan: 12 m
- Cruise speed: 120 kt / 220 km/h
- Characteristics: Maximum aerodynamic efficiency, sporty handling, emission-free and quiet operation, Swiss-made engineering