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NASA Tiltduct (concept design)

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

(Image credit: NASA Ames Research Center)

Tiltduct (concept design)
NASA Ames Research Center
Moffett Field, California, USA
www.nasa.gov/ames

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.

NASA's Distributed Electric Propulsion (DEP) research
NASA started researching distributed electric propulsion (DEP) on 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 tail-sitter 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 models 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 2026, NASA's space probes have not traveled to any other solar systems in the Milky Way galaxy, yet.

NASA Ames Research Center, NASA Langley and Johns Hopkins Applied Physics Laboratory eVTOL contributions
All electric common reference models (eCRM) designs came from the NASA Ames Research Center. The Greased Lightning drone, the LA-8 testbed, the Puffin (concept design and subscale prototype), the Raven (Research Aircraft for eVTOL Enabling Technologies) concept design and the Raven-Swft (Subscale Wind-Tunnel and Flight Test model) subscale technology demonstrator were designed and built in NASA Langley. The Johns Hopkins Applied Physics Laboratory (APL) is the primary facility responsible for designing and building the Dragonfly eVTOL space probe.

Mark Moore statement on Distributed Electric Propulsion (DEP)
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 distributed electric propulsion, "There has not been this pace in aeronautics since the Wright Brothers."

NASA Tiltduct passenger eVTOL aircraft (concept design)
The NASA Tiltduct is a six passenger eVTOL tilt-ducted fan concept design aircraft that can accept battery packs 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 of the aircraft is estimated at 174 mph (280 km/h) and the aircraft is recommended to have a reserve for cruise power for 20 minutes. The aircraft has six tilting-ducted propellers and has six electric motors. Starting from the front of the aircraft, there are two tilt-ducted fans on a canard wing, two tilting-ducted fans 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 aircraft has canard wings with one short front wing and one high main wing. There is a rear vertical stabilizer and a horizontal stabilizer. If you notice, it is difficult to see the front wing, the entire high main wing and the rear horizontal stabilizer. If you notice, the wings and the horizontal stabilizer are attached permanently to the rear of rotating ducted fans. As the ducted fan tilts, so does that portion of the wing that is attached to the rear of the ducted fan.

The aircraft's fuselage looks similar to a conventional general aviation airplane with the exception of the large tilting-ducted fans. The fuselage is made from carbon fiber composite for a high strength and low weight ratio. 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

NASA Advanced Air Mobility Playbook
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 Ames Research Center)

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 tilting-ducted fans
  • Electric motors: 6 electric motors (or the number of electric motors could be doubled for more power and redundancy depending upon the customers request or the manufacturer)
  • Power source: Battery packs 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 wings (1 short front wing and 1 high main wing)
  • Tail: 1 vertical stabilizer, 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.

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