United Kingdom HUMA

The HUMA is a Powered Lift eVTOL aircraft developed by Samad Aerospace in London, United Kingdom. It is currently in the Initial Design phase. It also has a cruise speed of 201 units, and a range of 161 units. For more information on this aircraft, see their website.

Last updated on February 26th, 2024.

Characteristics

General
NameHUMA
CompanySamad Aerospace
IndustryStart-ups
CityLondon
CountryUnited Kingdom
Primary ClassificationPowered Lift
Secondary ClassificationVectored Thrust
Tertiary ClassificationInclined Sitter
Energy SourceBattery
Capacity
Pilot typePiloted
AnnouncedMarch 2019
First (Unmanned) Flight
First (Manned) Flight
Design MaturityInitial Design
Official Websitehttp://www.samadaerospace.com/
Geometry
Length
Height
Span
Wing ConfigurationConventional
Wing sweep?No
Seating
seat
Seating Configuration seat
Passenger Seat Rows
Seats per Row
Separated pilot seat?Yes
Seating LayoutStandard
Performance
Max Take-off Weight (MTOW)
Operating Empty Weight (OEW)
Payload200 kg
Battery Mass
Cruise Speed108.5 kt
Max Speed
Range86.9 nm
Endurance
Cruise Altitude
Max Altitude
Thrust
Power Available
Propulsors
Propulsor TypeProp
Propulsor Layout
Total Number of Propulsors1
Propulsors in Cruise1
Propulsor in Hover1
Individual Propulsor Thrust
Individual Propulsor Power
Electric Energy
Battery Capacity
Battery Power
Battery Density
Battery Current0.00
Battery Voltage
Battery Chemical System
Battery Charge Time
Battery Charge Rate
Charging Voltage
Maneuverability
Wheeled Ground Taxi?
Independent Ground Taxi?
Conventional Landing?
Amphibious?