Comparison of P-80 variants

The following table compares the variants of the Lockheed P-80 Shooting Star.

XP-80

XP-80A/P-80A/F-80

Description

Role

Single-seat fighter

Crew

Pilot

First flight

January 8, 1944

June 10, 1944

Manufacturer

Lockheed Corporation

Production total

1

1,715

Dimensions

Length

32 ft 10 in (10.01 m)

34 ft 5 in (10.49 m)

Wingspan

37 ft (11.28 m)

38 ft 9 in (11.81 m)

Height

10 ft 3 in (3.12 m)

11 ft 3 in (3.43 m)

Wing area

240 ft² (22.30 m²)

237.6 ft² (22.07 m²)

Weights

Empty weight

6,287 lb (2,852 kg)

8,420 lb (3,819 kg)

Max. takeoff weight

8,916 lb (4044 kg)

16,856 lb (7646 kg)

Powerplant

Engine

One dH H.1B Goblin turbojet

One Allison J33-A-35 turbojet

Thrust

5,400 lbf (24.0 kN)

Performance

Maximum speed

502 mph (808 km/h)

600 mph (966 km/h)

Cruise speed

410 mph (660 km/h)

Range

Unknown

1,200 mi (1,930 km)

Service ceiling

41,000 ft (12,500 m)

46,000 ft (14,000 m)

Rate of climb

3,000 ft/min (920 m/min)

3,000 ft/min (920 m/min)

Armament

Guns

6 X .50 cal (12.7 mm) machine guns

Bombs

2 x 1000 lb (450 kg) bombs

Rockets

10x to 16x rockets

See also

  • List of World War II jet aircraft
  • List of Lockheed aircraft