hi
experimental engine releasing in the 2030's that uses on open fan structure
12 fan blades, 12 stationary guide vanes, all with variable pitch
maximum pitch
minimum pitch
fan blades are derived from REW's turbofan
VTOL for guide vane pitch, Trim for fan blade pitch
NASA X-66A using these engines out april 3rdish
thanks
Specifications
Spotlights
- PlaneFlightX 8 months ago
- RicardoACE 8 months ago
- Zerkk 8 months ago
General Characteristics
- Successors 2 airplane(s) +14 bonus
- Created On Windows
- Wingspan 16.4ft (5.0m)
- Length 20.3ft (6.2m)
- Height 39.5ft (12.0m)
- Empty Weight 192,870lbs (87,484kg)
- Loaded Weight 235,405lbs (106,778kg)
Performance
- Power/Weight Ratio 0.286
- Wing Loading N/A
- Wing Area 0.0ft2 (0.0m2)
- Drag Points 18892
Parts
- Number of Parts 812
- Control Surfaces 0
- Performance Cost 2,259
That will be used on the A380 as a testbed engine.
The avgeek see this :no no no
Me : ok
@JuliaAircraft hes just a lil guy
My favorite open rotor engine
@Mal0ne he's cute though:(
@SomeAircraftGuy @JuliaAircraft leave him alone guys ;(
yup, each fan blade is like 45 parts
very goofy engine
810+ parts per engine?
@GXSTATS yessir !
A380 Flying laboratory engine?
@Timplanes essentially the only difference will be the engines :)
@Mal0ne phew! 😅 Don’t know if I’ll be able to run the high part version, but I’m excited nonetheless
wieord engine i love it
@Timplanes we're looking at 3.8k rn but i can push out a 1.6k ish version for sure
the part count on that X-66 gonna be cRaZY