Our Projects

Up to the challenge

SF-600 e-Power

SF600A e-Power is an advanced, full electric cargo-feeder aircraft

Under study in collaboration with Vulcan Air and DESA, would be the first european light commercial electric aircraft CS-23 certified, zero emissions for short range freight transport, designed for high value and time demanding goods and merchandise.

Preliminary design is at an advanced stage, first flight expected by first quarter 2025.

The original SF600A is a fixed wing cargo aircraft designed to operate in difficult geographical areas, by 2025, there will be a huge demand for zero-emission cargo aircraft, but very few products are really available, we have seen the opportunity to upgrade the existing SF600A and attract customers and investors on this new market niche.

The zero-emission “SF600A e-Power” is designed to provide a flight time of 120 minutes, including CS-23 reserves, sufficient to perform more than 80% of the aircraft’s current missions while maintaining the current payload.

Two 400-kW electric powertrains (2 electric engine of 200KW each) will replace the aircraft’s Allison piston engines, and 1600 kg (3.527 lb.) of battery pack (almost 1000 KWh) will be stored in the belly pod under the fuselage (based on the most recent Li-Ion technology ).

Turnaround time should be comparable to the aircraft powered by Avgas. This electric propulsion project will allow saving more than 40% direct operating cost (DOC) per plane per year in 2025 vs conventional similar aircraft, with no CO2 emission. 

The conversion will be certified through a Supplemental Type Certificate (STC) and is expected to pay back with current energy prices in ten years and six years with self-produced energy via photovoltaic fields with its storage systems. In short, we want a new aircraft with zero emissions and a faster return on investment.

AG- 01

An  advanced electric air vehicle for Urban Air Mobility

  • FULL ELECTRIC – (10 small size engines, with energy recovery systems for batteries recharging and range increase)
  • VERTICAL TAKE-OFF AND LANDING  (to enable runway independent operations)
  • HIGH LEVEL OF FLIGHT AUTOMATION  (up to and including full automation , self-piloted)
  • AIRCRAFT-LIKE CRUISE
  • QUAD-ROTOR DUCTED FAN – WING EMBEDDED (Distributed electric propulsion with multiple redundant propellers or fans,  not rotorwings,  equipped with parachute systems)
  • OPERATIONALLY MID-WAY HELICOPTER-AIRCRAFT (helicopter at TO and Landing, Aircraft in cruise)
     

AG-01 will be equipped with:

  • 4 fans embedded in the wing and 1 installed over-the-wing
  •  the wing produces lift during cruise therefore reducing the power overall energy demand 

AG-01 will have twin-engine configuration that is: 

  • 8 engines will be installed in 4 couples on the same axis,  
  • during take-off and landing each of couple will activate a fan that generate vertical thrust
  • during cruise only the additional engines couple over-the-wing  will generate thrust while the other could be used to recharge the batteries in case of need 

S.A.F.E.

Silent Airplane Free of Emissions

The project concerns the design of a 40-80 seat up to 1000 km range Silent Aircraft Free from Emissions (SAFE).  The words “silent” and “emissions-free” are rather relative to current standards, as encapsulated in the following aircraft characteristics:

  • Inaudible outside airport boundaries, that is below the noise level of average road traffic, 
  • Emissions-free below 900m altitude using only electric power for the take-off and landing phases;
  • Carbon-free cruise flight powered by ducted fans driven by turbines with LH fuel;
  • SAF may be used for turbines as an alternative to LH for carbon-neutral flight;
  • High-level of operational flexibility with triple power sources (turbines, batteries, fuel cells) and dual fuels (LH and SAF);
  • Design allows replacement by more advanced batteries (solid state), fuel cells and turbine to improve performance and efficiency;
  • Blended Wing Body (BWB) configuration with large volume for the cabin with windows and cargo hold;
  • Cargo hold for interchangeable freight containers or LH tanks allowing payload range flexibility;
  • Overwing engine exhaust for noise shielding;
  • STOL performance allows the use of 1000m runways for take-off and precision landing with MLS/SatNav;
  • Prevention of contrail formation and associated greenhouse gas effects by altitude adjustment in cruise integrated with ATM;
  • Good revenue potential for passengers and cargo operating from hubs or regional airport;
  • Design for sustainability and low life-cycle cost,