• +1-703-684-6777
  • See footer

NASA Tiltduct (concept design)

NASA Tiltduct passenger eVTOL concept design aircraft (Image credit: NASA)

 

Tiltduct (concept design)
NASA
Washington, D.C., USA
www.nasa.gov

Established in 1958, the National Aeronautics and Space Administration (NASA) is an independent agency of the U.S. federal government responsible for the civil space program, aeronautics research and space research. NASA is headquartered in Washington, D.C. and has 10 major field centers. NASA has made space ships, explored space, the moon, launched satellites, gathered data about Earth from space, made the Skylab Space Station, explored Mars, studied our solar system using space probes and more. (Image credit: NASA)

NASA started researching distributed electric propulsion (DEP) electric vertical takeoff and landing (eVTOL) and hybrid-electric VTOL aircraft in 2009. DEP was introduced to the world in November 2009 when Mark Moore, while still at NASA, unveiled the Puffin, a personal an all-battery eVTOL concept design aircraft. For the first time, the world caught a glimpse at how electric propulsion might transform everyday flight. In 2010, according to one website, the first eVTOL aircraft flown was NASA's Puffin subscale eVTOL tailsitting aircraft.

In 2014, NASA built both eVTOL and fixed-wing DEP technology demonstrator aircraft. Some of the key design features for NASA's advanced air mobility (AAM) common reference vehicles is to increase safety exponentially, reduce the complexity of the aircraft, decrease the cost of manufacturing, minimize maintenance costs, lower the final ticket cost to the consumer, lessen or have no carbon footprint for the aircraft and decrease the noise level for the general public.

NASA has continued making passenger eVTOL concept designs, technology demonstrators and research eVTOL aircraft for any company that wants to take advantage of NASA's research. In addition, NASA is now making eVTOL and hybrid-electric eVTOL aircraft to explore planets and their moons, in our solar system. As of 2024, NASA's space probes have not traveled to any other solar systems in the Milky Way galaxy, yet.

Mark Moore, Co-Founder and CEO of Whisper Aero (formerly a Principal Investigator and Chief Technologist for On-Demand Mobility, NASA and Engineering Director of Aviation, Uber Elevate) at the Vertical Flight Society's 7th Annual Electric VTOL Symposium, Jan. 21-23, 2020 in San Jose, California, USA, stated concerning advanced air mobility (AAM), "There has not been this pace in aeronautics since the Wright Brothers."

NASA Tiltduct passenger eVTOL concept design aircraft
The NASA Tiltduct is a six passenger eVTOL tilt-ducted fan (or propeller) concept design aircraft that can accept all-batteries as a power source or use a hybrid-electric power source. NASA calls this concept design aircraft an Urban Air Mobility (UAM) reference vehicle, also known as a common reference model. The aircraft has two distinct modes of flight, helicopter and cruise flight. The aircraft is either piloted or uses autonomous piloting. The aircraft has large windows providing spectacular views for the pilot and passengers.

The cruise speed is estimated at 174 mph (280 km/h) and the aircraft is recommended to have reserve cruise power for 20 minutes. The aircraft has six tilt-ducted propellers and has six (or 12) electric motors. Starting from the front of the aircraft, there are two tilt-ducted propellers on a canard wing, two tilt-ducted propellers at the end of a high main wing and two tilt-ducted propellers on the tail's horizontal stabilizer.

The estimated empty weight of the aircraft is 5,889 lb (2,672 kg), has an anticipated maximum payload weight 1,200 lb (544 kg) and has a forecasted maximum takeoff weight of 7,089 lb (3,216 kg). The fuselage is made from carbon fiber composite for a high strength and low weight ratio. The aircraft's fuselage looks similar to a conventional general aviation airplane with the exception of the large tilt-duted propellers. The aircraft has one tail fin (or vertical stabilizer) and has one horizontal stabilizer. The aircraft has fixed tricycle wheeled landing gear.

NASA advanced air mobility (AAM) aircraft research areas:

  • Aircraft Design
  • Noise and Annoyance
  • Operational Effectiveness
  • Performance
  • Propulsion Efficiency
  • Rotor-Rotor Interactions
  • Rotor-Wing Interactions
  • Safety and Airworthiness
  • Structure and Aeroelasticity

NASA's advanced air mobility (AAM) facilities and capabilities include:

  • Air Traffic Operations Lab
  • Airspace Operations Lab
  • Ames UAM Lab
  • CERTAIN Range
  • Cockpit Motion Facility
  • Cognitive Engineering Lab
  • Computational Fluid Dynamics
  • Developmental UAM Simulator - Flyer
  • Dryden Aeronautical Test Range
  • Exterior Effects Room
  • Flight Loads Lab
  • Future Flight Central
  • Icing Research
  • Landing and Impact Research Facility
  • Low Speed Aeroacoustic Wind Tunnel
  • Mobile Acoustics Facility
  • Mobile Operations Facility
  • Research Flight Deck
  • Testbed Virtual Infrastructure
  • UAS Flight Test Control Room
  • Vertical Motion Simulator
  • X-57 Maxwell
  • 12' Tunnel-Low-Cost Exploratory Facility
  • 14 by 22 Foot Subsonic Tunnel

In February 2023, NASA published an article title, "NASA is Creating an Advanced Air Mobility Playbook." NASA is working with academia, government agencies, industry, cities and tribal nations to make advanced air mobility (AAM) a reality. NASA's areas of support include accessibility, automation, cargo delivery, emergency response, future airspace, healthcare, infrastructure, noise, ride quality, safety, travel time, vertiports and more.

NASA Tiltduct Urban Air Mobility (UAM) Reference Vehicle orthographic view illustrations with hover and cruise configurations shown (Image credit: NASA)

NASA Tiltduct Urban Air Mobility (UAM) Reference Vehicle orthographic view illustrations with hover and cruise configurations shown (Image credit: NASA)

Specifications:

  • Aircraft type: Passenger eVTOL concept design aircraft
  • Piloting: Unknown, possibly piloted or autonomous
  • Capacity: 6 passengers
  • Cruise speed: 174 mph (280 km/h)
  • Reserve cruise power: 20 minutes
  • Empty weight, estimated: 5,889 lb (2,672 kg)
  • Maximum payload weight, estimated: 1,200 lb (544 kg)
  • Maximum takeoff weight, estimated: 7,089 lb (3,216 kg)
  • Propellers: 6 tilt ducts (8 VTOL-only propellers, 1 pusher propeller for forward flight)
  • Electric motors: 6 electric motors (or double the amount depending upon the manufacturer)
  • Power source: All batteries or a hybrid-electric power source
  • Fuselage: Carbon fiber composite
  • Windows: Panoramic wrap around windows allowing forward, left and right visibility for spectacular views with a solid roof above
  • Wings: 1 canard and 1 main high wing
  • Tail: 1 tail fin (or vertical stabilizer) and 1 horizontal stabilizer
  • Landing gear: Fixed tricycle wheeled landing gear
  • Safety features: Distributed Electric Propulsion (DEP) means having multiple propellers (or electric ducted fans) and multiple electric motors on an aircraft so if one or more propellers (or electric ducted fans) or some electric motors fail, the other working propellers (or electric ducted fans) and electric motors can safely land the aircraft. DEP provides safety through redundancy for passengers or cargo. There are also redundancies of critical components in the sub-systems of the aircraft providing safety through redundancy. Having multiple redundant systems on any aircraft decreases having any single point of failure.

Related Aircraft:

Company Insights:

Resources: