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Help could arrive by air, when every minute makes a difference

Air ambulance
Future design concepts for the TANNANA family

What you need could arrive through smoother, faster air cargo

Air cargo
Future design concepts for the TANNANA family

Scientific expeditions could reach further, opening new horizons for research

Flying research laboratory
Future design concepts for the TANNANA family

You could camp somewhere you never imagined reaching

Flying camper
Future design concepts for the TANNANA family

The joy of riding could stay with you… this time in the air

Personal flying motorcycle
Future design concepts for the TANNANA family

Your daily journey from home to work could begin… with flight

TANNANA CROW
Future design concepts for the TANNANA family
Explore CROW

TANNANA is a family of flying vehicles in development, designed to combine vertical take-off and landing, hovering and flexible directional control. We designed it around the Humming Propulsion System, developed over more than a decade, to open new possibilities for travel and exploration. Its capabilities and operating limits will be established through development and testing. This is the idea behind its name…

TANNANA

TANNANA CROW

Our first TANNANA

The two-seat TANNANA CROW is our first crewed model in development, intended to become the first crewed flying vehicle powered by the Humming Propulsion System. Four propulsion units, two occupants within a 200 kg target payload, and a target maximum take-off weight of one tonne

A target speed of up to 500 km/h and a range of up to 1,000 km, powered by hydrogen and batteries

TANNANA CROW: a two-seat cabin and four Humming Propulsion units
TANNANA CROW · HPS Aviation design visualisation of a vehicle in development

Choose a number to explore its details

More of your time for the journey

A target maximum speed of up to 500 km/h. During forward flight, the lifting body is designed to reduce the lift demanded from the propulsion units

Target maximum speed
Up to 500 km/h
Target cruise speed
300 km/h
Target operating altitude
Up to 10,000 ft
Take-off & landing
Vertical, with an oblique climb path where operating conditions permit
Forward flight
Progressive transition to aerodynamic lift as airspeed increases
Lift at cruise speed
Body designed to target full aircraft weight support through aerodynamic lift at 300 km/h

Figures describe the current design and its targets; final performance is established through testing and certification

Get to know CROW up close

Change the view and select a part directly in the image to explore its function and specifications

TANNANA CROW — Front perspectiveHumming PropulsionHumming PropulsionHumming PropulsionHumming PropulsionLifting body & airframeCabin & payloadControl & safety

Humming Propulsion

Four propulsion units are being developed to manage lift, acceleration, braking and manoeuvring by directing thrust, coordinated by the vehicle control system

Main propulsion units
4
Force direction
Change the resultant thrust direction within the unit
View all specifications

The specifications shown are design targets derived from the propulsion specifications

Flight and parking scenario

The journey starts with your destination

In the intended operating concept, once you board TANNANA and enter your destination, an air traffic coordination algorithm plans the shortest available route while coordinating movement to avoid conflicts with other flight paths. TANNANA’s flexibility in low-altitude flight and hovering close to the ground offers more movement options within permitted areas and altitudes. Where air passage is unavailable, ground manoeuvring within operating areas is considered to reach a suitable stopping and parking location

We design for preparation, take-off, flight and landing, followed by manoeuvring to parking. Each stage brings operating and testing requirements into the vehicle programme

What happens after landing?

Manoeuvre to the parking space

TANNANA is being developed to manoeuvre from its landing point to suitable parking within the operating area. The path depends on its external dimensions and available manoeuvring space

Positioning and parking that support the flight

Air approach
AIRLANDAB
  1. 01Air approach
  2. 02Landing
  3. 03Manoeuvring & parking

Illustration of journey modes, not a simulation of operating speeds or flight angles

Safety provisions

When we talk about flight, safety is the first concern for users and certification authorities. That is why we develop TANNANA around complementary layers of protection covering propulsion, control, energy and landing options. These systems are part of the design and development programme; testing establishes their performance and operating limits

Multiple channels within each propulsion unit

Three operating channels in each propulsion unit, each with its own motor and controller, distribute operation within the system

Multi-channel control systems

Multiple control paths are being developed to coordinate propulsion units and manage the vehicle’s response if a path fails

Primary and reserve energy

Hydrogen fuel cells work with batteries, with power and energy reserves managed for flight and landing requirements

Emergency parachute descent

Four rescue parachutes within the target design are intended to support emergency descent within altitude and speed limits established by testing

Landing on land

A target capability to land at suitable, permitted sites, accounting for space, surface conditions and operating limits

Landing on water

An additional landing option in the design, subject to validation of buoyancy, stability and water-surface conditions

Continuous system-health monitoring

Monitoring propulsion, energy and control behaviour to identify unusual indications and support an appropriate response

Fault isolation

Operating-path independence and isolation of failed components are studied to limit the spread of a fault through the system

Thrust redistribution

The control system coordinates available units and channels to support balance and manoeuvring within the remaining capability

Flight-envelope protection

Simpler user tasks alongside operating-limit monitoring, energy-reserve management and selection of a suitable landing path

Energy for the range Power for take-off

Hydrogen and batteries in one architecture, managing the demands of each phase of the journey

Power for take-off

Batteries support peak demand during take-off and manoeuvring alongside the fuel cells. Energy management coordinates demand with reserves and system health

How does power become movement?
H₂

Fuel cells

Sustained power support

Batteries

Peak-demand support

Energy management and power distribution
HPS01
HPS02
HPS03
HPS04

Four propulsion units · Illustration of system roles

How is this possible?

The Humming Propulsion System is the innovation that opened the way to this concept. For more than a decade, we have rethought a system that combines propulsion, lift and steering, and developed TANNANA around it

What is the Humming Propulsion System?
Humming Propulsion System