|
Lockheed P-80 Shooting Star
|
1944 |
 |
Lockheed -Lockheed Martin |
| Aircraft on photo: Lockheed P-80A Shooting Star Photo source: US Air Force via Wikipedia |
|
| Data for: F-80C |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
933 km/h |
(580 mph) |
Length: |
| Type: |
jet fighter |
Range: |
2.221 km |
(1.380 mi) |
Span: |
| Description: |
first jet fighter used operationally by USAF |
Ceiling: |
14.000 m |
(46.000 mi) |
Height: |
| First flight: |
1944 |
Rate of climb: |
23,2 m/s |
(4.580 ft/min) |
Max weight: |
| Crew: |
1 |
|
|
|
Number built: |
|
| 10,52 m |
(34 ft 6 in) |
| 11,81 m |
(38 ft 9 in) |
| 3,43 m |
(11 ft 3 in) |
| 7.646 kg |
(16.856 lb) |
| 1.715 |
|
|
| Engine: |
1 x Allison J-33 turbojet |
|
|
| Thrust: |
1 x 20,46 kN (1 x 4.600 lbf) |
|
More info: |
| Armament: |
Guns: 6 x 12,7 mm (6 x 0.50 in) |
|
Wikipedia |
| |
Rockets: 8 (unguided) |
|
National Museum |
| |
Bombs: 2 x 454 kg (2 x 1.000 lb) |
|
|
|
| |
| Sources: |
| Jane's Encyclopedia of |
| Aviation, Crescent Books, |
| 1993 |
|
|
|
|
|
Lockheed EF-80 Shooting Star
|
1944 |
 |
|
| Aircraft on photo: Lockheed EF-80A Shooting Star Photo source: crimso.msk.ru |
|
| |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
NA |
|
Length: |
| Type: |
experimental fighter |
Range: |
NA |
|
Span: |
| Description: |
prone pilot test aircraft |
Ceiling: |
NA |
|
Height: |
| First flight: |
1944 |
Rate of climb: |
NA |
|
Max weight: |
| Crew: |
2 |
|
|
|
Number built: |
|
| NA |
|
| 11,81 m |
(38 ft 9 in) |
| 3,43 m |
(11 ft 3 in) |
| NA |
|
| 1 |
|
|
| Engine: |
1 x Allison J-33 turbojet |
|
More info / sources: |
| Thrust: |
1 x 20,46 kN (1 x 4.600 lbf) |
|
|
| Armament: |
NA |
|
|
|
|
|
|
|
|
Lockheed F-80 Trijet
|
1947 |
 |
|
| Aircraft on photo: Lockheed F-80 Trijet Photo source: Flying, September 1952 (magazine) |
|
| |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed |
|
|
Length: |
| Type: |
experimental fighter |
(ramjet only): |
800 km/h |
(500 mph) |
Span: |
| Description: |
first manned airplane powered by ramjet alone |
Range: |
NA |
|
Height: |
| First flight: |
1947 |
Ceiling: |
NA |
|
Max weight: |
| Crew: |
1 |
Rate of climb: |
NA |
|
Number built: |
|
| 10,52 m |
(34 ft 6 in) |
| NA |
|
| 3,43 m |
(11 ft 3 in) |
| NA |
|
| 2 |
|
|
| Engine: |
1 x Allison J-33 turbojet |
|
More info: |
| |
2 x Marquardt C30 ramjets |
|
Joe Baugher |
| Thrust: |
1 x 20,46 kN (1 x 4.600 lbf) Allison |
|
Airwar |
| |
2 x 21,8 kN (2 x 4.900 lbf) Marquardt |
|
Avia Deja Vu |
| Armament: |
NA |
|
Source: |
|
|
|
|
|
|
Lockheed F-94 Starfire
|
1949 |
 |
|
| Aircraft on photo: Lockheed YF-94A Starfire Photo source: National Museum of the US Air Force |
|
| Data for: F-94A |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
970 km/h |
(600 mph) |
Length: |
| Type: |
interceptor |
Range: |
1.064 km |
(660 mi) |
Span: |
| Description: |
1st USAF all-weather interceptor jet |
Ferry range: |
1.500 km |
(930 mi) |
Height: |
| First flight: |
1949 |
Ceiling: |
15.500 m |
(50.850 ft) |
Max weight: |
| Crew: |
2 |
Rate of climb: |
34 m/s |
(6.740 ft/min) |
Number built: |
|
| 12,23 m |
(40 ft 1 in) |
| 11,87 m |
(38 ft 9 in) |
| 3,86 m |
(12 ft 8 in) |
| 7.645 kg |
(16.854 lb) |
| 855 |
(total F-94) |
|
Engine:
|
1 x Allison J-33 turbojet |
|
|
| Thrust: |
1 x 19,5 kN (1 x 4.385 lbf) dry thrust |
|
|
| |
1 x 26,6 kN (1 x 5.980 lbf) with afterburner |
|
|
| Armament: |
Guns: 4 x 12,7 mm (4 x 0.50 in) |
|
|
|
|
|
|
|
|
Lockheed YF-94C Starfire early
|
1950 |
 |
|
| Aircraft on photo: Lockheed YF-94C Starfire early Photo source: National Museum of the US Air Force |
|
| (also called Lockheed YF-97A) |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
942 km/h |
(585 mph) |
Length: |
| Type: |
interceptor prototype
|
Range: |
1.296 km |
(805 mi) |
Span: |
| Description: |
F-94C prototype with a new wing, swept tail
|
Ferry range: |
NA |
|
Height: |
| |
plane and new engine (license built Rolls
|
Ceiling: |
15.666 m |
(51.400 ft) |
Max weight: |
| |
Royce Tay) vs F-94A |
Climb rate: |
40,5 m/s |
(7.980 ft/min)
|
Number built: |
| First flight: |
1950 |
Crew: |
2 |
|
|
|
| 12,23 m |
(40 ft 1 in) |
| 12,9 m |
(42 ft 5 in) |
| 4,5 m |
(14 ft 11 in) |
10.975 kg
|
(24.200 lb) |
| 2 |
|
| More info |
/sources: |
|
Engine:
|
1 x Pratt & Whitney J48-P-3 turbojet |
|
| Thrust: |
1 x 26,7 kN (1 x 6,000 lbf) dry thrust |
|
| |
1 x 35,6 kN (1 x 8,000 lbf) with afterburner |
|
| Armament: |
none |
|
|
|
|
|
|
|
Lockheed YF-94C Starfire late
|
1950 |
 |
|
| Aircraft on photo: Lockheed YF-94C Starfire late Photo source: Kev's Military Aviation Pics |
|
| (also called Lockheed YF-97A) |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
942 km/h |
(585 mph) |
Length: |
| Type: |
interceptor prototype
|
Range: |
1.296 km |
(805 mi) |
Span: |
| Description: |
later YF-94C with new nose having rockets
|
Ferry range: |
NA |
|
Height: |
| |
armament placed around the radome and |
Ceiling: |
15.666 m |
(51.400 ft) |
Max weight: |
| |
covered by snap-action doors |
Climb rate: |
40,5 m/s |
(7.980 ft/min)
|
Number built: |
| First flight: |
1950 |
Crew: |
2 |
|
|
|
| 13,5 m |
(44 ft 6 in) |
| 12,9 m |
(42 ft 5 in) |
| 4,5 m |
(14 ft 11 in) |
10.975 kg
|
(24.200 lb) |
| 2 |
|
| More info |
/sources: |
|
Engine:
|
1 x Pratt & Whitney J48-P-3 turbojet |
|
| Thrust: |
1 x 26,7 kN (1 x 6,000 lbf) dry thrust |
|
| |
1 x 35,6 kN (1 x 8,000 lbf) with afterburner |
|
| Armament: |
Rockets: 24 x 70 mm (24 x 2.75 in) surrounding the radome
|
|
|
|
|
|
|
|
Lockheed F-94C Starfire
|
1950 |
 |
|
| Aircraft on photo: Lockheed F-94C Starfire Photo source: National Museum of the US Air Force |
|
| Data for: F-94C |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
1.030 km/h |
(640 mph) |
Length: |
| Type: |
interceptor |
Range: |
1.300 km |
(810 mi) |
Span: |
| Description: |
F-94 development with longer nose, swept tail, |
Fer. range: |
1.921 km |
(1.200 mi) |
Height: |
| |
radome surrounded with 24 rockets and
|
Ceiling: |
15.670 m |
(51.400 ft) |
Max weight: |
| |
12-rocket pods mounted on wings leading edges |
Climb rate: |
40,5 m/s |
(7.980 ft/min) |
Numb. built: |
| First flight: |
1950 (YF-94C)
|
Crew: |
2 |
|
|
|
| 13,56 m |
(44 ft 6 in) |
| 12,93 m |
(42 ft 5 in) |
| 4,50 m |
(14 ft 11 in) |
| 10.977 kg |
(24.200 lb) |
| 387 |
(F-94C) |
| |
|
|
Engine:
|
1 x Pratt & Whitney J48 turbojet |
|
Thrust:
|
1 x 28,2 kN (1 x 6.350 lbf) dry thrust |
More info: |
| |
1 x 38,92 kN (1 x 8.750 lbf) with afterburner
|
Wikipedia |
| Armament: |
48 x 70 mm (48 x 2.75 in) air-to-air rockets |
Aviastar |
| |
(24 rockets around nose radome) |
|
|
| |
| Sources: |
| Jane's Encyclopedia of |
| Aviation, Crescent Books, |
| 1993 |
|
|
|
|
|
Lockheed YF-94D Starfire
|
1951 |
 |
|
| Aircraft on photo: Lockheed F-94B-5-LO modified as YF-94D Starfire Photo source: Flickr, Robert Sullivan |
|
| Data for: YF-94D |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
1.030 km/h |
(640 mph) |
Length: |
| Type: |
fighter-bomber |
Range: |
|
|
Span: |
| Description: |
single seater F-94 with 50% larger wing |
Ceiling: |
15.670 m |
(51.400 mi) |
Height: |
| First flight: |
1951 |
Rate of climb: |
40,5 m/s |
(7.980 ft/min) |
Max weight: |
| Crew: |
1 |
|
|
|
Number built: |
|
| NA |
|
| NA |
|
| 4,50 m |
(14 ft 11 in) |
| NA |
|
| 1 |
(unfinished) |
|
Engine:
|
1 x Pratt & Whitney J48 turbojet |
More info: |
Thrust:
|
1 x 28,2 kN (1 x 6.350 lbf) dry thrust |
|
|
1 x 38,92 kN (1 x 8.750 lbf) with afterburner
|
Sources: |
| Armament: |
Guns: 8 x 12,7 mm (8 x 0.50 in) |
|
| |
Hardpoints capacity: 1.800 kg (3.970 lb) |
|
|
|
|
|
|
|
Lockheed XF-90
|
1949 |
 |
|
| Aircraft on photo: Lockheed XF-90 Photo source: National Geographic via Flickr, twm1340 |
|
| |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
1.064 km/h |
(665 mph) |
Length: |
| Type: |
fighter prototype |
Range: |
3.680 km |
(2.300 mi) |
Span: |
| Description: |
penetration fighter & bomber escort |
Ceiling: |
11.890 m |
(39.000 ft) |
Height: |
| First flight: |
1949 |
Rate of climb: |
28,2 m/s |
(5.555 ft/min) |
Max weight: |
| Crew: |
1 |
|
|
|
Number built: |
|
| 17,12 m |
(56 ft 2 in) |
| 12,20 m |
(40 ft 0 in) |
| 4,80 m |
(15 ft 9 in) |
| 14.118 kg |
(31.060 lb) |
| 2 |
|
|
| Engines: |
2 x Westinghouse J34 turbojets |
|
| Thrust: |
2 x 18,2 kN (2 x 4.100 lbf) |
|
| Armament: |
Guns: 6 x 20 mm (6 x 0.79 in) |
|
| |
Rockets: 8 x 127 mm (8 x 5 in) |
|
| |
Bombs: 907 kg (2.000 lb) |
|
|
|
|
|
|
|
Lockheed F-104 Starfighter
|
1954 |
 |
|
| Aircraft on photo: Lockheed XF-104 Starfighter Photo source: National Museum of the US Air Force |
|
| Data for: F-104G |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
2.125 km/h |
(1.328 mph) |
Length: |
| Type: |
interceptor aircraft, fighter-bomber |
Combat radius: |
670 km |
(420 mi) |
Span: |
| Description: |
high performance supersonic interceptor |
Ferry range: |
2.623 km |
(1.630 mi) |
Height: |
| First flight: |
1954 |
Ceiling: |
15.000 m |
(50.000 ft) |
Max weight: |
| Crew: |
1 |
Rate of climb: |
244 m/s |
(48.000 ft/min) |
Number built: |
|
| 16,66 m |
(54 ft 8 in) |
| 6,36 m |
(21 ft 9 in) |
| 4,09 m |
(13 ft 6 in) |
| 13.170 kg |
(29.027 lb) |
| 2.575 |
(total F-104) |
|
| Engine: |
1 x General Electric J79 turbojet |
|
| Thrust: |
1 x 48 kN (1 x 10.000 lbf) dry thrust |
|
| |
1 x 69 kN (1 x 15.600 lbf) with afterburner |
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
| |
Hardpoints: 7 |
|
| |
Hardpoints capacity: 1.814 kg (4.000 lb) |
|
|
|
|
|
|
|
Lockheed F-104B/D Starfighter
|
1957 |
 |
|
| Aircraft on photo: Lockheed CF-104D Starfighter |
|
| Data for: F-104D |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
2.556 km/h |
(1.590 mph) |
Length: |
| Type: |
interceptor aircraft, fighter-bomber |
Range: |
2.414 km |
(1.500 mi) |
Span: |
| Description: |
F-104 combat capable 2-place trainer vers. |
Ceiling: |
17.700 km |
(58.000 ft) |
Height: |
| First flight: |
1957 |
Rate of climb: |
274 m/s |
(54.000 ft/min) |
Max weight: |
| Crew: |
2 |
|
|
|
Number built: |
|
| 16,68 m |
(54 ft 8 in) |
| 6,68 m |
(21 ft 11 in) |
| 4,11 m |
(13 ft 6 in) |
| 12.634 kg |
(27.850 lb) |
| 26 (F-104B), |
21 (F-104D) |
|
| Engine: |
1 x General Electric J79 turbojet |
|
| Thrust: |
1 x 48 kN (1 x 10.000 lbf) dry thrust |
|
| |
1 x 69 kN (1 x 15.600 lbf) with afterburner |
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
| |
Hardpoints: 7 |
|
| |
Hardpoints capacity: 1.814 kg (4.000 lb) |
|
|
|
|
|
|
|
Lockheed NF-104A Starfighter
|
1963 |
 |
|
| Aircraft on photo: Lockheed NF-104A Starfighter Photo source: Avia Deja Vu |
|
| |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
+ 2,4 M |
|
Length: |
| Type: |
aerospace trainer |
Range: |
NA |
|
Span: |
| Description: |
X-15 mixed power low cost astronaut trainer |
Ferry range: |
NA |
|
Height: |
| First flight: |
1963 |
Ceiling: |
36.800 m |
(120.800 ft) |
Max weight: |
| Crew: |
1 |
Rate of climb: |
NA |
|
Number built: |
|
| NA |
|
| 7,84 m |
(25 ft 9 in) |
| 4,11 m |
(13 ft 6 in) |
| 9.890 kg |
(21.400 lb) |
| 3 |
|
|
| Engines: |
1 x General Electric J79 turbojet |
|
| |
1 x Rocketdyne AR2 liquid fueled rocket engine |
|
| Thrust: |
GE: 1 x 43,54 kN (1 x 9.600 lbf) |
|
| |
Rocketdyne: 1 x 27,2 kN (1 x 6.000 lbf) |
|
| Armament: |
none |
|
|
|
|
|
|
|
Lockheed YF-12
|
1963 |
 |
|
| Aircraft on photo: Lockheed YF-12A Photo source: National Museum of the US Air Force |
|
| |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
3.661 km/h |
(2.275 mph) |
Length: |
| Type: |
interceptor |
Combat radius: |
2.000 km |
(1.250 mi) |
Span: |
| Description: |
developed from A-12, followed by SR-71 |
Ferry range: |
4.800 km |
(3.000 mi) |
Height: |
| First flight: |
1963 |
Ceiling: |
27.400 m |
(90.000 ft) |
Max weight: |
| Crew: |
2 |
Rate of climb: |
NA |
|
Number built: |
|
| 30,97 m |
(101 ft 8 in) |
| 16,95 m |
(55 ft 7 in) |
| 5,64 m |
(18 ft 6 in) |
| 56.200 kg |
(124.000 lb) |
| 3 |
|
|
| Engines: |
2 x Pratt & Whitney J58 high-bypass-ratio turbojet with afterburner (turbo/ramjet hybrid) |
|
| Thrust: |
2 x 91,2 kN (2 x 20.500 lbf) dry thrust |
|
| |
2 x 140 kN (2 x 31.500 lbf) with afterburner |
|
| Armament: |
3 x air-to-air missiles in fuselage bays |
|
|
|
|
|
|
|
Lockheed CL-1200
|
1970 |
 |
|
| Aircraft on photo: Lockheed CL-1200 Photo source: i-f-s.nl |
|
| |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
2.720 km/h |
(1.700 mph) |
Length: |
| Type: |
interceptor |
Combat radius: |
680 km |
(420 mi) |
Span: |
| Description: |
improved F-104 and F-5E competitor |
Ferry range: |
2.000 km |
(1.250 mi) |
Height: |
| First flight: |
1970 (estimate) |
Ceiling: |
18.300 m |
(60.000 ft) |
Max weight: |
| Crew: |
1 |
Rate of climb: |
305 m/s |
(60.000 ft/min) |
Number built: |
|
| 17,45 m |
(57 ft 3 in) |
| 8,89 m |
(29 ft 2 in) |
| 5,23 m |
(17 ft 2 in) |
| 15.900 kg |
(35.000 lb) |
| 2 |
|
|
| Engine: |
1 x Pratt & Whitney TF-30 turbofan |
|
|
| Thrust: |
1 x 66,7 kN (1 x 15.000 lbf) dry thrust |
|
|
| |
1 x 111,2 kN (1 x 25.000 lbf) with afterburner |
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) or 1 x30 mm (1 x 1.18 in) |
|
|
| |
Hardpoints: 9 |
|
|
| |
Hardpoints capacity: 5.450 kg (12.000 lb) |
|
|
|
|
|
|
|
|
Lockheed X-27 Lancer (mock up)
|
1972 |
 |
|
| Aircraft on photo: Lockheed X-27 Lancer Photo source: Roadrunnersinternationale.com |
|
| |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
2.330 km/h |
(1.450 mph) |
Length: |
| Type: |
lightweight fighter |
Combat radius: |
NA |
|
Span: |
| Description: |
derived from CL-1200 Lancer |
Ferry range: |
3.400 km |
(2.100 mi) |
Height: |
| Cancelled: |
1972 |
Ceiling: |
18.300 m |
(60.000 ft) |
Max weight: |
| Crew: |
1 |
Rate of climb: |
NA |
|
Number built: |
|
| 16,2 m |
(53 ft 2 in) |
| 8,7 m |
(28 ft 7 in) |
| 4,9 m |
(16 ft 2 in) |
| 16.000 kg |
(35.200 lb) |
| 1 |
(mock up) |
|
| Engine: |
1 x Pratt & Whitney TF-30 turbofan |
|
|
| Thrust: |
NA |
|
|
| Armament: |
NA |
|
|
| |
|
|
|
|
|
|
|
|
|
Lockheed XST Have Blue
|
1977 |
 |
|
| Aircraft on photo: Lockheed XST Have Blue Photo source: F-117a.com |
|
| |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
970 km/h |
(600 mph) |
Length: |
| Type: |
technology demonstrator |
Range: |
970 km |
(600 mi) |
Span: |
| Description: |
F-117 forerunner |
Ceiling: |
NA |
|
Height: |
| First flight: |
1977 |
Rate of climb: |
NA |
|
Max weight: |
| Crew: |
1 |
|
|
|
Number built: |
|
| 14,4 m |
(47 ft 3 in) |
| 6,8 m |
(22 ft 6 in) |
| 2,33 m |
(7 ft 6,25 in) |
| 5.670 kg |
(12.500 lb) |
| 2 |
|
|
| Engines: |
2 x General Electric J85 turbojets |
|
|
| Thrust: |
2 x13,4 kN (2 x 2.950 lbf) |
|
|
| Armament: |
none |
|
|
|
|
|
|
|
|
Lockheed F-117 Nighthawk
|
1981 |
 |
|
| Aircraft on photo: Lockheed F-117A Nighthawk |
|
| |
|
| Manufacturer: |
Lockheed Corporation, USA |
Max speed: |
993 km/h |
(617 mph) |
Length: |
| Type: |
stealth ground attack aircraft |
Range: |
1.720 km |
(1.070 mi) |
Span: |
| Description: |
first operational stealth aircraft |
Ceiling: |
20.000 m |
(69.000 ft) |
Height: |
| First flight: |
1981 |
Rate of climb: |
NA |
|
Max weight: |
| Crew: |
1 |
|
|
|
Number built: |
|
| 20,09 m |
(65 ft 11 in) |
| 13,20 m |
(43 ft 4 in) |
| 3,78 m |
(12 ft 9,5 in) |
| 23.800 kg |
(52.500 lb) |
| 64 |
|
|
| Engines: |
2 x General Electric F404 turbofans |
|
|
| Thrust: |
2 x 48 kN (2 x 10.600 lbf) |
|
|
| Armament: |
2 x internal weapons bays (1 hardpoint each) |
|
|
|
|
|
|
|
|
Lockheed YF-22
|
1990 |
 |
|
| Aircraft on photo: Lockheed YF-22 Photo source: National Museum of the US Air Force |
|
| |
|
| Manufacturer: |
Lockheed/Boeing/General Dynamics, USA |
Max speed: |
2.655 km/h |
(1.650 mph) |
Length: |
| Type: |
prototype fighter |
Range: |
NA |
|
Span: |
| Description: |
ATF Advanced Tactical Fighter winner |
Ferry range: |
3.704 km |
(2.300 mi) |
Height: |
| First flight: |
1990 |
Ceiling: |
NA |
|
Max weight: |
| Crew: |
1 |
Rate of climb: |
NA |
|
Number built: |
|
| 19,56 m |
(64 ft 2 in) |
| 13,11 m |
(43 ft 0 in) |
| 5,36 m |
(17 ft 7 in) |
| 28.123 kg |
(62.000 lb) |
| 2 |
|
|
| Engines: |
2 x Pratt & Whitney F119-P-100 augmented turbofans |
|
|
| Thrust: |
2 x 104 kN (2 x 23.500 lbf) dry thrust |
|
|
| |
2 x 156,8 kN (2 x 34.600 lbf) with afterburner |
|
|
| Armament: |
Guns: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
Missiles: 6 in internal bays + 4 on external hardpoints |
|
|
|
|
|
|
|
|
Lockheed Martin F-22 Raptor
|
1997 |
 |
|
| Aircraft on photo: Lockheed Martin F-22A Raptor |
|
| |
|
| Manufacturer: |
Lockheed Martin / Boeing USA |
Max speed: |
2.410 km/h |
(1.500 mph) |
Length: |
| Type: |
stealth air superiority fighter |
Range: |
2.960 km |
(1.840 mi) |
Span: |
| Description: |
5th generation twin engine stealth fighter |
Ferry range: |
3.219 km |
(2.000 mi) |
Height: |
| First flight: |
1997 |
Ceiling: |
19.812 m |
(65.000 ft) |
Max weight: |
| Crew: |
1 |
Rate of climb: |
NA |
|
Number built: |
|
| 18,90 m |
(62 ft 0 in) |
| 13,56 m |
(44 ft 6 in) |
| 5,08 m |
(16 ft 8 in) |
| 38.000 kg |
(83.500 lb) |
| 166 |
(Sep. 2010) |
|
| Engines: |
2 x Pratt & Whitney F119-PW-100 Pitch Thrust vectoring augmented turbofans |
|
|
| Thrust: |
2 x 104 kN (2 x 23.500 lbf) dry thrust |
|
|
| |
2 x 156,8 kN (2 x 34.600 lbf) with afterburner |
|
|
| Armament: |
Guns: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
Missiles: 8 in internal bays + 4 on external hardpoints |
|
|
|
|
|
|
|
|
Lockheed Martin X-35
|
2000 |
 |
|
| Aircraft on photo: Lockheed Martin X-35A Photo source: Lockheed Martin |
|
| Data for: X-35B |
|
| Manufacturer: |
Lockheed/Northrop (USA), BAE (UK) |
Max speed: |
1.930 km/h |
(1.200 mph) |
Length: |
| Type: |
prototype/demonstrator |
Combat radius: |
1.000 km |
(622 mi) |
Span: |
| Description: |
JSF Joint Strike Fighter program winner |
Ferry range: |
2.222 km |
(1.380 mi) |
Height: |
| First flight: |
2000 |
Ceiling: |
+15.240 m |
(+50.000 ft) |
Max weight: |
| Crew: |
1 |
Rate of climb: |
classified |
|
Number built: |
|
| 15,37 m |
(50 ft 6 in) |
| 10,65 m |
(35 ft 0 in) |
| 5,28 m |
(17 ft 4 in) |
| 27.220 kg |
(60.000 lb) |
| 2 |
|
|
| Engines: |
1 x Pratt & Whitney F135 afterburning turbofan coupled to Rolls-Royce lift system |
|
|
| Thrust: |
1 x 128 kN (1 x 28.000 lbf) P&W dry thrust |
|
|
| |
1 x 191 kN (1 x 43.000 lbf) P&W afterburner thrust |
|
|
| |
1 x 80 kN (1 x 18.000 lbf) RR lift thrust |
|
|
| Armament: |
none |
|
|
|
|
|
|
|
|
Lockheed Martin F-35A Lightning II
|
2006 |
 |
|
| Aircraft on photo: Lockheed Martin F-35A Lightning II Photo source: Lockheed Martin |
|
| |
|
| Manufacturer: |
Lockheed Martin Aeronautics, USA |
Max speed: |
2.065 km/h |
(1.283 mph) |
Length: |
| Type: |
stealth multirole fighter |
Combat radius: |
1.090 km |
(677 mi) |
Span: |
| Description: |
5th generation, single seat, single engine |
Ferry range: |
2.222 km |
(1.380 mi) |
Height: |
| First flight: |
2006 |
Ceiling: |
18.288 m |
(60.000 ft) |
Max weight: |
| Crew: |
1 |
Rate of climb: |
classified |
|
Number built: |
|
| 15,67 m |
(51 ft 4 in) |
| 10,70 m |
(35 ft 0 in) |
| 4,33 m |
(14 ft 2 in) |
| 31.800 kg |
(70.000 lb) |
| 15 |
(preproduction) |
|
| Engine: |
1 x Pratt & Whitney F135 afterburning turbofan |
|
|
| Thrust: |
1 x 128 kN (1 x 28.000 lbf) dry thrust |
|
|
| |
1 x 191 kN (1 x 43.000 lbf) with afterburner |
|
|
| Armament: |
Gun: 1 x 25 mm (1 x 0.98 in) or 1 x 30 mm (1 x 1.18 in) |
|
|
| |
Hardpoints: 6 external + 4 internal |
|
|
| |
Hardpoints capacity: 8.100 kg (18.000 lb) |
|
|
|
|
|
|
|
|
Lockheed Martin F-35B Lightning II
|
2008 |
 |
|
| Aircraft on photo: Lockheed Martin F-35B Lightning II (STOVL) Photo source: Lockheed Martin |
|
| |
|
| Manufacturer: |
Lockheed Martin Aeronautics, USA |
Max speed: |
2.065 km/h |
(1.283 mph) |
Length: |
| Type: |
stealth multirole fighter |
Combat radius: |
833 km |
(520 mi) |
Span: |
| Description: |
short take off and vertical landing STOVL |
Ferry range: |
1.670 km |
(1.040 mi) |
Height: |
| First flight: |
2008 |
Ceiling: |
18.288 m |
(60.000 ft) |
Max weight: |
| Crew: |
1 |
Rate of climb: |
classified |
|
Number built: |
|
| 15,6 m |
(51 ft 3 in) |
| 10,7 m |
(35 ft 0 in) |
| 4,33 m |
(14 ft 2 in) |
| 27.000 kg |
(60.000 lb) |
| 15 |
(preproduction) |
|
| Engines: |
1 x Pratt & Whitney F135 afterburning turbofan coupled to Rolls-Royce lift system |
|
|
| Thrust: |
1 x 128 kN (1 x 28.000 lbf) P&W dry thrust |
|
|
| |
1 x 191 kN (1 x 43.000 lbf) P&W afterburner thrust |
|
|
| |
1 x 80 kN (1 x 18.000 lbf) RR lift thrust |
|
|
| Armament: |
Gun: 1 x 25 mm (1 x 0.98 in) or 1 x 30 mm (1 x 1.18 in) |
|
|
| |
Hardpoints: 6 external + 4 internal |
|
|
| |
Hardpoints capacity: 8.100 kg (18.000 lb) |
|
|
|
|
|
|
|
|
Lockheed Martin F-35C Lightning II
|
2010 |
 |
|
| Aircraft on photo: Lockheed Martin F-35C Lightning II Photo source: Lockheed Martin |
|
| |
|
| Manufacturer: |
Lockheed Martin Aeronautics, USA |
Max speed: |
2.065 km/h |
(1.283 mph) |
Length: |
| Type: |
stealth multirole fighter |
Range: |
1.185 km |
(740 mi) |
Span: |
| Description: |
naval version-folding wings & larger span |
Ferry range: |
2.520 km |
(1.565 mi) |
Height: |
| First flight: |
2010 |
Ceiling: |
18.288 m |
(60.000 ft) |
Max weight: |
| Crew: |
1 |
Rate of climb: |
classified |
|
Number built: |
|
| 15,7 m |
(51 ft 5 in) |
| 13,1 m |
(43 ft 0 in) |
| 4,54 m |
(14 ft 9 in) |
| 31.800 kg |
(70.000 lb) |
| 15 |
(preproduction) |
|
| Engine: |
1 x Pratt & Whitney F135 afterburning turbofan |
|
|
| Thrust: |
1 x 128 kN (1 x 28.000 lbf) dry thrust |
|
|
| |
1 x 191 kN (1 x 43.000 lbf) with afterburner |
|
|
| Armament: |
Gun: 1 x 25 mm (1 x 0.98 in) or 1 x 30 mm (1 x 1.18 in) |
|
|
| |
Hardpoints: 6 external + 4 internal |
|
|
| |
Hardpoints capacity: 8.100 kg (18.000 lb) |
|
|
|
|
| |
|