Very cool.

However, I would be interested in seeing the pros and cons of it vs the Bell/Agusta BA609 and/or the V-22 Osprey.

BA609

General characteristics
Crew: 1 or 2
Capacity: 6 to 9 passengers/5,500 pounds (2,500 kg) payload
Length: 44 ft (13.3 m)
Rotor diameter: ()
Height: 16 ft 3 in (5.1 m) nacelles vertical; (21 ft 10 in (6.6 m) nacelles horizontal
Wingspan: 38 ft 5 in (11.7 m)
Width with rotors: 60 ft 5 in (14.1 m)
Rotor diameter: 25 ft 10 in (7.92 m))
Disc area: 981.75 ft² (98.53 m²)
Empty weight: 10,483 lb (4,765 kg)
Useful load: 5,500 lb (2,500 kg)
Max takeoff weight: 16,800 lb (7,600 kg)
Powerplant: 2× Pratt & Whitney Canada PT6C-67A turboshaft, 1,940 hp (1,447 kW) each
Performance
Maximum speed: 275 knots (315 mph, 510 km/h)
Cruise speed: 260 knots (299 mph, 465 km/h)
Range: 750 nmi (852 mi, 1,390 km)
Service ceiling: 25,000 ft (7,620 m)
Rate of climb: 1,500 ft/min (7.62 m/s)
Disc loading: 15.8 lb/sq ft (77 kg/m²)