Some info on the 262/P-80 numbers I found in a quick search. P-80 listed under 262.
Engine: Two 1,986 lb (900 kg) thrust Junkers Jumo 004B axial flow Turbojets
One 4500lb (2,041kg) thrust Allison J33-A-21 turbojet.
Wing Span: 41 ft 1 in (12.5 m)
38 ft 9 in (11.81 m)
Length: 34 ft 8.5 in (10.58 m)
34 ft (10.49 m)
Height: 12 ft 6.75 in (3.83 m)
11 ft 4 in (3.45 m)
Weight: Empty 8,820 lb (4,000 kg)
Empty 8,176 lb (3,709 kg)
Loaded 14,938 lb (7,045 kg)
Gross 11,700 lb (5,350), Max T/O 14,000 lb (6,350)
Maximum Speed: 540 mph at 19,685 ft (870 km/h at 6,000 m)
577 mph (929 km/h) at 6,000 ft (1,830 m)
558 mph at sea level
492 mph at 40,000 ft
Ceiling: 37,664 ft (11,450 m )
45,000 ft (13,716 m)
Range: 650 miles (1,050 km)
780/1,440 miles (1,255km/2,317 km)
Climb Rate: 3,937 ft/min (1,200 m/min)
4,580 ft/min (1,396 m/min)
Armament: Four 30 mm MK108 cannons in nose, two with 100 rounds each, two with 80; could also carry 24 R4M 55 mm unguided rockets on
underwing racks.
P-80: Six .50cal mgs, 2,000 lbs bombs, 10 rockets (5 in?)