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Lancer Epav

The Lancer Epav is a Powered Lift eVTOL aircraft developed by Esprit Aeronautics in London, United Kingdom. It is currently in the Scaled Prototype phase. The Lancer Epav aircraft has a capacity of one (1) occupant. For more information on this aircraft, see their website.

Last updated on February 24th, 2025.

Characteristics

General
Name	Lancer Epav
Company	Esprit Aeronautics
Industry	Start-ups
City	London
Country	United Kingdom
Primary Classification	Powered Lift
Secondary Classification	Separate Thrust
Tertiary Classification	Lift + Cruise
Energy Source	Hybrid-Electric
Capacity	1 seat
Pilot type	Piloted
Announced	January 2018
First (Unmanned) Flight
First (Manned) Flight
Design Maturity	Scaled Prototype
Official Website	https://www.espritaero.com/epav-vtol

Geometry
Length
Height
Span
Wing Configuration	Conventional
Wing sweep?	No

Seating

Seating Configuration	1 seat
Passenger Seat Rows
Seats per Row
Separated pilot seat?	Yes
Seating Layout	Standard

Performance
Max Take-off Weight (MTOW)
Operating Empty Weight (OEW)
Payload	120 kg
Battery Mass
Cruise Speed
Max Speed	78.3 kt
Range
Endurance	100 min
Cruise Altitude
Max Altitude
Thrust
Power Available

Propulsors
Propulsor Type	Prop
Propulsor Layout
Total Number of Propulsors	8
Propulsors in Cruise
Propulsor in Hover	8
Individual Propulsor Thrust
Individual Propulsor Power	30 kW

Electric Energy
Battery Capacity
Battery Power
Battery Density
Battery Current	0.00
Battery Voltage
Battery Chemical System
Battery Charge Time
Battery Charge Rate
Charging Voltage

Maneuverability
Wheeled Ground Taxi?	No
Independent Ground Taxi?
Conventional Landing?
Amphibious?