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Compiled by the editorial staff of eVTOL.com

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Samad Aerospace reveals concept for Q-Starling personal air vehicle

Samad Aerospace has shared more about its plans for a two-seat, hybrid-electric personal VTOL aircraft, which it is calling the Q-Starling.

Samad Aerospace Q-Starling
The hybrid-electric Q-Starling design incorporates elements from both fast jets and VTOL aircraft. Samad Aerospace Image

The U.K.-based eVTOL developer announced last year that it would be spinning off a two-seat version of the half-scale prototype of its e-Starling air taxi. Chief technology officer Norman Wijker said that not only does the Q-Starling “[exist] on its own merits, but the experience will put [Samad Aerospace] at the head of the game when it comes to e-Starling development and certification and is consequently a major strategic advantage.”

According to a brochure for the aircraft, the Q-Starling will have a length of just over and a wingspan of just under eight meters (26 feet) and a maximum take-off weight of around 1,040 kilograms (2,300 pounds). It will cruise at 250 knots (460 kilometers per hour) and have a range of 500 miles (800 km). Its anticipated service ceiling is 15,000 feet (4,570 m).

Q-Starling will hover using the thrust of a single large-diameter fan, while Reaction Control System (RCS) fans in the wing and tailplane maintain control and balance. The fly-by-wire aircraft features a single side-stick controller, through which the pilot will be able to command all three axes of rotation, plus vertical and forward movement.

Samad propulsion system
Q-Starling will be powered by a hybrid-electric turbo-generator which will provide power for a large diameter hover fan and forward thrust once the aircraft has transitioned from vertical flight. Samad Aerospace Image

On approach, VTOL controls will kick in at just above the stall speed of 65 knots (120 km/h), activating the RCS. The main fan doors will open, the flaps will deploy, the landing gear will lower, and the fan will begin to power up and start off-loading the wing.

Samad Aerospace said the Q-Starling will incorporate “numerous and extensive safety systems” to prevent the aircraft from departing the flight envelope, allowing it to be flown by private pilots with only around 10 hours of additional training. The aircraft will also have a ballistic parachute system as an extra safety measure.

The hybrid-electric propulsion system will incorporate two modified PBS TS100 turboshafts rated at 180 kilowatts (241 horsepower). They will be capable of running on bio-diesel/sustainable aviation fuel and be backed up by batteries during the take-off and landing phases.

Samad Q-Starling above clouds
Samad Aerospace aims for the Q-Starling to be “less time-consuming than any plane or train and as luxurious as a private jet, at less than half of its operating cost.” Samad Aerospace Image

Targeted squarely at the high end of the personal aviation market, the Q-Starling won’t necessarily demand the kind of volume manufacturing that will be required to make eVTOL air taxis commercially viable, Wijker suggested. As the designer of the Q-Starling, he said, “knowing that costs were not a major consideration was extremely liberating, as it allowed me the use of the best materials, and the best technologies to produce something that any wealthy owner would be proud to own.”

Samad Aerospace CEO Dr. Seyed Mohseni described the Q-Starling as “the ultimate luxury in personal hybrid-electric flying,” giving passengers “unparalleled point-to-point mobility options” while also being “efficient and sustainable.”

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5 Comments

  1. This design seems to have considered ceritifaction, hover power optimisation and and luxury elements simultaneously.
    Well done to Dr Seyed M Mohseni and CTO Norman Widjker for this amazing peace of engineering and art.

  2. As I continue to marvel in it’s design, it becomes clearer that this aircraft is in a sophisticated class of it’s own. As the name implies, it embodies an avian impression. The Q-Starling is a piece of art that even Rembrandt would be entranced with. I can only imagine the complex engineering that must have been associated with the graceful design. I cannot stop gazing at it. Absolutely gorgeous in all respects. To all whom worked on it, I would like to say congratulations on an aircraft above and before all. Thank you.

  3. With such small diameter (2 m ?) single rotor to elevate 1040 kg, the needed power could be around 700 HP, and the downwash below it about 50 m/s!
    Also to keep the internal cabin sound level just bearable will be not a simple task and humingbird will be a better name for this bird.

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