| Swift | |
|---|---|
Artist's conception | |
| General information | |
| Type | Aerobatic two seat light aircraft |
| National origin | United Kingdom |
| Manufacturer | Swift Aircraft |
| History | |
| First flight | Expected late 2023 [1] |
The Swift Aircraft Swift is a single engine, conventional light aircraft, seating two in side-by-side configuration. It is being developed in the UK but has yet to fly.
The Swift is mostly built from composite materials; flying surfaces and the fuselage are formed from composite sandwiches and the wing and tailplane have carbon fibre spars. It has a low wing of trapezoidal plan with slightly upturned tips, fitted with Frise ailerons and slotted flaps. The rear surfaces are also trapezoidal. There is a trim tab in the elevator and a ground adjustable tab on the rudder. [2]
The cockpit has a fixed windscreen and rearward-sliding canopy and is equipped with dual controls. There is a baggage space behind the side-by-side seats. The Swift has a fixed, tricycle undercarriage with the mainwheels on fuselage mounted, spring steel, cantilever legs. The mainwheels have disc brakes and the nosewheel is steerable. The Swift is designed to accept a range of Textron Lycoming horizontally opposed engines in the power range 119–194 kW (160–260 hp), driving a three-bladed propeller. [2]
The Swift program was announced in May 2009. In 2015 Swift Technology Group announced a "multi million pound investment" supporting development of the aircraft and other products, [3] [4] and exhibited a static display at AeroExpo UK. [5]
In 2021, the Royal Air Force announced its intention to become carbon neutral, called Project MONET. [6] To further this project, the UK MOD awarded a contract in 2023 to develop the Swift as a zero-emission aircraft with a possible implementation date of 2027. [7] Swift Technology Group have begun experimenting with hemp and flax fibres in the composite panels, [1] as well as alternate fuels, and even electric propulsion. [7]
Data from Jane's All the World's Aircraft 2011/12 [2] Performance estimated.
General characteristics
Performance
Avionics