Lockheed Martin F-35 Lightning IISpecifications (F-35A)

General characteristics

Crew: 1 Length: 51.4 ft (15.67 m) Wingspan: 35 ft[N 5] (10.7 m) Height: 14.2 ft[N 6] (4.33 m) Wing area: 460 ft²[258] (42.7 m²) Empty weight: 29,300 lb (13,300 kg) Loaded weight: 49,540 lb[242][N 7][507] (22,470 kg) Max. takeoff weight: 70,000 lb[N 8] (31,800 kg) Powerplant: 1 × Pratt & Whitney F135 afterburning turbofan

Dry thrust: 28,000 lbf[508][N 9] (125 kN)

Thrust with afterburner: 43,000 lbf[508][509] (191 kN) Internal fuel capacity: 18,480 lb (8,382 kg)[N 10]

Performance

Maximum speed: Mach 1.6+[262] (1,200 mph, 1,930 km/h) (tested to Mach 1.61)[376]

Range: 1,200 nmi (2,220 km)on internal fuel Combat radius: 584 nmi[510] (1,080 km)on internal fuel[511]

Service ceiling: 60,000 ft[512] (18,288 m) (tested to 43,000 ft)[513]

Rate of climb: classified (not publicly available) Wing loading: 107.7 lb/ft² (526 kg/m²; 745 kg/m² max loaded) Thrust/weight: **With full fuel: 0.87

With 50% fuel: 1.07 Max g-limits: 9 g[N 11]

Lockheed Martin F-22 RaptorSpecifications

General characteristics

Crew: 1 Length: 62 ft 1 in (18.90 m) Wingspan: 44 ft 6 in (13.56 m) Height: 16 ft 8 in (5.08 m) Wing area: 840 ft² (78.04 m²) Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip Empty weight: 43,340 lb (19,700 kg[6][285])

Loaded weight: 64,460 lb (29,300 kg[N 5]) Max. takeoff weight: 83,500 lb (38,000 kg) Powerplant: 2 × Pratt & Whitney F119-PW-100 Pitch Thrust vectoring turbofans

Dry thrust: 23,500 lb[288] (104 kN) each

Thrust with afterburner: 35,000+ lb[6][288] (156+ kN) each Fuel capacity: 18,000 lb (8,200 kg) internally,[6][285] or 26,000 lb (11,900 kg) with two external fuel

tanks.[6][285] About 3,050 gal or 20,333 lb JP-8 (without additions) internally.[289]

Performance

Maximum speed: **At altitude: Mach 2.25 (1,500 mph, 2,410 km/h) [estimated][124]

Supercruise: Mach 1.82 (1,220 mph, 1,963 km/h)[124]

Range: >1,600 nmi (1,840 mi, 2,960 km)with 2 external fuel tanks Combat radius: 410 nmi (with 100 nmi in supercruise)[284] (471 mi, 759 km) Ferry range: 2,000 mi(1,738 nmi, 3,219 km) Service ceiling: >65,000 ft [290] (19,812 m) Wing loading: 77 lb/ft² (375 kg/m²) Thrust/weight: 1.09 (1.26 with loaded weight & 50% fuel) Maximum design g-load: -3.0/+9.0 g[124]

Lockheed YF-12General characteristics

Crew: 2 Length: 101 ft 8 in (30.97 m) Wingspan: 55 ft 7 in (16.95 m) Height: 18 ft 6 in (5.64 m) Wing area: 1,795 ft² (167 m²) Empty weight: 60,730 lb (27,604 kg) Loaded weight: 124,000 lb (56,200 kg[6]) Max. takeoff weight: 140,000 lb (63,504 kg) Powerplant: 2 × Pratt & Whitney J58/JTD11D-20A high-bypass-ratio turbojet with afterburner

Dry thrust: 20,500 lbf (91.2 kN) each

Thrust with afterburner: 31,500 lbf (140 kN) each

Performance

Maximum speed: Mach 3.35 (2,275 mph, 3,661 km/h[6]) at 80,000 ft (24,400 m) Range: 3,000 mi (4,800 km) Service ceiling: 90,000 ft (27,400 m)

Lockheed F-104 StarfighterSpecifications (F-104G)

General characteristics

Crew: 1 Length: 54 ft 8 in (16.66 m) Wingspan: 21 ft 9 in (6.36 m) Height: 13 ft 6 in (4.09 m) Wing area: 196.1 ft² (18.22 m²) Airfoil: Biconvex 3.36% root and tip Empty weight: 14,000 lb (6,350 kg) Loaded weight: 20,640 lb (9,365 kg) Max. takeoff weight: 29,027 lb (13,170 kg) Powerplant: 1 × General Electric J79-GE-11A afterburning turbojet

Dry thrust: 10,000 lbf (48 kN)

Thrust with afterburner: 15,600 lbf (69 kN) Zero-lift drag coefficient: 0.0172 Drag area: 3.37 sq ft (0.31 m²) Aspect ratio: 2.45

Performance

Maximum speed: 1,328 mph (Mach 2.01, 1,154 kn, 2,137 km/h) Combat radius: 420 mi (365 nmi, 670 km) Ferry range: 1,630 mi(1,420 nm, 2,623 km) Service ceiling: 50,000 ft (15,000 m) Rate of climb: 48,000 ft/min (244 m/s) Wing loading: 105 lb/ft² (514 kg/m²) Thrust/weight: 0.54 with max. takeoff weight (0.76 loaded) Lift-to-drag ratio: 9.2

Lockheed F-94 StarfireSpecifications (F-94C Starfire)

General characteristics

Crew: 2 Length: 44 ft 6 in (13.6 m) Wingspan: 42 ft 5 in (12.9 m) Height: 14 ft 11 in (4.5 m) Wing area: 232.8 ft² (21.63 m²) Empty weight: 12,708 lb (5,764 kg)

Loaded weight: 18,300 lb (8,300 kg) Max. takeoff weight: 24,184 lb (10,970 kg) Powerplant: 1 × Pratt & Whitney J48-P-5 turbojet

Dry thrust: 6,350 lbf (28.2 kN)

Thrust with afterburner: 8,750 lbf (38.9 kN)

Performance

Maximum speed: 640 mph (556 kn, 1,030 km/h,Mach .84) Range: 805 mi (700 nmi, 1,300 km)combat Ferry range: 1,275 mi(1,100 nmi, 2,050 km) Service ceiling: 51,400 ft (15,670 m) Rate of climb: 7,980 ft/min (40.5 m/s) Wing loading: 78.6 lb/ft² (384 kg/m²) Thrust/weight: 0.48

Lockheed P-80 Shooting StarSpecifications (P-80C/F-80C)

General characteristics

Crew: One Length: 34 ft 5 in (10.49 m) Wingspan: 38 ft 9 in (11.81 m) Height: 11 ft 3 in (3.43 m) Wing area: 237.6 ft² (22.07 m²) Aspect ratio: 6.37 Empty weight: 8,420 lb (3,819 kg) Loaded weight: 12,650 lb (5,738 kg) Max. takeoff weight: 16,856 lb (7,646 kg) Powerplant: 1 × Allison J33-A-35 centrifugal compressor turbojet, 5,400 lbf (24.0 kN) Zero-lift drag coefficient : 0.0134 Drag area: 3.2 ft² (0.30 m²)

Performance

Maximum speed: 600 mph, Mach .76 (P-80A 558 mph at sea level and 492 mph at 40,000 ft)[7] (965 km/h)

Cruise speed: 410 mph (660 km/h) Range: 1,200 mi (1,930 km) Service ceiling: 46,000 ft (14,000 m) Rate of climb: 4,580 ft/min (23.3 m/s) 5.5 min to 20,000 ft (6,100 m) Wing loading: 53 lb/ft² (260 kg/m²) Thrust/weight: 0.43

Lift-to-drag ratio: 17.7

Lockheed P-38 LightningGeneral characteristics

Crew: One Length: 37 ft 10 in (11.53 m) (11.53 m) Wingspan: 52 ft 0 in (15.85 m) (15.85 m) Height: 12 ft 10 in (3.91 m) (3.91 m) Wing area: 327.5 ft² (30.43 m²) Airfoil: NACA 23016 / NACA 4412 Empty weight: 12,800 lb[119] (5,800 kg) Loaded weight: 17,500 lb[119] (7,940 kg) Max. takeoff weight: 21,600 lb (9,798 kg) Powerplant: 2 × Allison V-1710-111/113 V-12 piston engine, 1,475 hp (1,100 kW) at 3,000rpm each Zero-lift drag coefficient: 0.0268[119]

Drag area: 8.78 ft² (0.82 m²)[119]

Aspect ratio: 8.26[119]

Performance

Maximum speed: 443 mph (712 km/h) on War Emergency Power: 1,725 hp at 64 inHG and 28,000 ft (8,530 m)[N 7][N 8][citation needed]

Stall speed: 105 mph (169 km/h) (170 km/h) Range: 1,300 mi (2,100 km) combat (1,770 km / 3,640 km) Service ceiling: 44,000 ft (13,000 m) (13,400 m) Rate of climb: 4,750 ft/min (24.1 m/s) maximum Wing loading: 53.4 lb/ft²[119] (260.9 kg/m²) Power/mass: 0.16 hp/lb (0.27 kW/kg) Lift-to-drag ratio: 13.5