Here's specs from the Wikipedia entry for Mitsubishi J2M (
https://en.wikipedia.org/wiki/Mitsubishi_J2M#Specifications)
Specifications
Data from Mitsubishi J2M3-21 Raiden
General characteristics
Crew: one, pilot
Length: 9.70 m (32 ft 8 in)
Wingspan: 10.80 m (35 ft 5 in)
Height: 3.81 m (13 ft 0 in)
Wing area: 20 m² (216 ft²)
Empty weight: 2,839 kg (6,259 lb)
Loaded weight: 3,211 kg (7,080 lb)
Powerplant: 1 × Mitsubishi MK4R-A Kasei 23a 14-cylinder two-row radial engine, 1,379 kW (1,850 hp)
Performance
Maximum speed: 596km/h (370 mph, 322kt) (@5450m)
Range: 560 km (302 nmi, 348 mi)
Service ceiling: 11,430 m (37,500 ft)
Rate of climb: 1402 m/min (4,600 ft/min)
Wing loading: 174 kg/m² (35 lb/ft²)
Power/mass: 0.42 kW/kg (0.26 hp/lb)
And for the Ki.61:
https://en.wikipedia.org/wiki/Kawasaki_Ki-61#Specifications_.28Ki-61-I-KAIc.29Specifications (Ki-61-I-KAIc)Data from Japanese Aircraft of the Pacific War
General characteristics
Crew: 1
Length: 8.94 m (29 ft 4 in)
Wingspan: 12 m (39 ft 4 in)
Height: 3.7 m (12 ft 2 in)
Wing area: 20 m2 (220 sq ft)
Airfoil: NACA 2R 16 wing root, NACA 24009 tip
Empty weight: 2,630 kg (5,798 lb)
Gross weight: 3,470 kg (7,650 lb)
Fuel capacity:
Internal 550 l (150 US gal; 120 imp gal)
External 2x 200 l (53 US gal; 44 imp gal)
Powerplant: 1 × Kawasaki Ha40 inverted liquid-cooled V-12 piston engine, 864 kW (1,159 hp)
Propellers: 3-bladed variable pitch propeller
Performance
Maximum speed: 580 km/h (360 mph; 313 kn) at 5,000 m (16,000 ft)
Range: 580 km (360 mi; 313 nmi)
Service ceiling: 11,600 m (38,100 ft)
Rate of climb: 15.2 m/s (2,990 ft/min)
Time to altitude: 7.0 min to 5,000 m (16,000 ft)
Wing loading: 173.5 kg/m2 (35.5 lb/sq ft)
Power/mass: 0.25 kW/kg (0.15 hp/lb)
I think that's our Ki.61, and it apparently sourced from Francillon. Not sure about the J2M3 specs