|
McDonnell FH-1 Phantom
|
1945 |
 |
McDonnell Douglas-Boeing |
Aircraft on photo: McDonnell FH-1 Phantom Photo source: Hudson Airdepot
|
|
| |
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
771 km/h
|
(479 mph)
|
Length: |
Type:
|
carrier based fighter aircraft |
Range: |
1.120 km
|
(695 mi)
|
Span:
|
Description:
|
first jet aircraft to land on US aircraft carrier |
Ferry range:
|
1.580 km
|
(980 mi)
|
Height:
|
First flight:
|
1945
|
Ceiling: |
12.525 m |
(41.100 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
21,5 m/s |
(4.230 ft/min) |
Number built: |
|
11,35 m
|
(37 ft 3 in)
|
12,42 m
|
(40 ft 9 in)
|
4,32 m
|
(14 ft 2 in)
|
5.459 kg
|
(12.035 lb)
|
62
|
|
|
| Engines: |
2 x Westinghouse J30 turbojets
|
|
|
Thrust:
|
2 x 7,1 kN (2 x 1.600 lbf)
|
|
|
| Armament: |
Guns: 4 x 12,7 mm (4 x 0.50 in)
|
|
|
|
|
|
|
|
McDonnell XF2H Banshee
|
1947 |
 |
|
| Aircraft on photo: McDonnell XF2D-1 Banshee Photo source: tailspintopics.blogspot.com |
|
Data for: XF2H-1
|
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
NA
|
|
Length: |
Type:
|
carrier-based fighter aircraft |
Range: |
NA |
|
Span:
|
Description:
|
one of primary US fighters in Korean War
|
Ferry range:
|
NA |
|
Height:
|
First flight:
|
1947
|
Ceiling: |
NA |
|
Max weight: |
Crew:
|
1
|
Rate of climb:
|
NA |
|
Number built: |
|
11,89 m
|
(39 ft 0 in)
|
12,69 m
|
(41 ft 7.4 in)
|
4,41 m
|
(14 ft 5.5 in)
|
NA
|
|
3
|
prototypes
|
|
| Engines: |
2 x Westinghouse J34 turbojets
|
|
|
Thrust:
|
2 x 13,34 kN (2 x 3.000 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
|
|
| |
|
|
McDonnell F2H Banshee
|
1949 |
 |
|
Aircraft on photo: McDonnell F2H-2 Banshee Photo source: NAS Sanford
|
|
Data for: F2H-1
|
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
945 km/h
|
(587 mph)
|
Length: |
Type:
|
carrier-based fighter aircraft |
Combat range: |
966 km
|
(600 mi)
|
Span:
|
Description:
|
XF2H with lengthened fuselage & more power |
Ferry range:
|
2.057 km
|
(1.278 mi)
|
Height:
|
First flight:
|
1949
|
Ceiling: |
14.728 m |
(48.500 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
37,5 m/s |
(7.380 ft/min)
|
Number built: |
|
12,24 m
|
(40 ft 1.8 in)
|
12,69 m
|
(41 ft 7.4 in)
|
4,41 m
|
(14 ft 5.5 in)
|
8.591 kg
|
(18.940 lb)
|
895
|
(total F2H) |
|
| Engines: |
2 x Westinghouse J34 turbojets
|
|
|
Thrust:
|
2 x 14 kN (2 x 3.150 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in) |
|
|
|
|
|
|
|
|
McDonnell F2H-2N Banshee
|
1950 |
 |
|
| Aircraft on photo: McDonnell F2H-2N Banshee Photo source: tailspintopics.blogspot.com |
|
| |
|
Manufacturer:
|
McDonnell Aircraft, USA
|
Max speed:
|
945 km/h
|
(587 mph)
|
Length: |
Type:
|
carrier-based night fighter aircraft |
Combat range: |
992 km
|
(620 mi)
|
Span:
|
Description:
|
F2H-2 with radar housed in lengthened nose |
Ferry range:
|
2.360 km
|
(1.475 mi)
|
Height:
|
First flight:
|
1950
|
Ceiling: |
14.728 m |
(48.500 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
37,5 m/s |
(7.380 ft/min)
|
Number built: |
|
13,10 m
|
(40 ft 1.8 in)
|
12,69 m
|
(41 ft 7.4 in)
|
4,41 m
|
(14 ft 5.5 in)
|
9.525 kg
|
(18.940 lb)
|
14
|
(total 895) |
|
| Engines: |
2 x Westinghouse J34 turbojets
|
|
|
Thrust:
|
2 x 14,5 kN (2 x 3.250 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in) |
|
|
| |
Bombs: 454 kg (1.000 lb) or Rockets: 6 x 127 mm (6 x 5 in) |
|
|
|
|
|
|
|
|
McDonnell F2H-3 Banshee
|
1952
|
 |
|
Aircraft on photo: McDonnell F2H-3 Banshee
|
|
| |
|
Manufacturer:
|
McDonnell Aircraft, USA
|
Max speed:
|
933 km/h
|
(580 mph)
|
Length: |
Type:
|
carrier-based all weather fighter aircraft |
Combat range: |
992 km
|
(620 mi)
|
Span:
|
Description:
|
F2H with lengthened fuselage & redesigned tail |
Ferry range:
|
2.760 km
|
(1.716 mi)
|
Height:
|
First flight:
|
1952
|
Ceiling: |
14.205 m |
(46.600 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
30 m/s |
(6.000 ft/min)
|
Number built: |
|
14,68 m
|
(48 ft 2 in)
|
12,73 m
|
(41 ft 9 in)
|
4,42 m
|
(14 ft 6 in)
|
11.437 kg
|
(25.214 lb)
|
250
|
(total 895) |
|
| Engines: |
2 x Westinghouse J34 turbojets
|
|
|
Thrust:
|
2 x 14,5 kN (2 x 3.250 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in) |
|
|
| |
Hardpoints: 8
|
|
|
| |
Hardpoints capacity: 1.415 kg (3.120 lb) of bombs, rockets or missiles
|
|
|
|
|
|
|
|
|
McDonnell XF-85 Goblin
|
1948 |
 |
|
Aircraft on photo: McDonnell XF-85 Goblin Photo source: Wikipedia
|
|
| |
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
1.069 km/h
|
(664 mph)
|
Length: |
Type:
|
parasite fighter |
Range: |
NA
|
|
Span:
|
Description:
|
conceived to be carried in B-36 bomb bay
|
Ferry range:
|
NA
|
|
Height:
|
First flight:
|
1948
|
Ceiling: |
14.600 m |
(48.000 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
63,3 m/s
|
(12.500 ft/min)
|
Number built: |
|
4,50 m
|
(14 ft 10 in)
|
6,40 m
|
(21 ft 1 in)
|
2,50 m
|
(8 ft 3 in)
|
2.540 kg
|
(5.600 lb)
|
2
|
|
|
| Engines: |
1 x Westinghouse XJ34 turbojet
|
|
|
Thrust:
|
1 x 13,3 kN (1 x 3.000 lbf)
|
|
|
| Armament: |
Guns: 4 x 12,7 mm (4 x 0.50 in)
|
|
|
| |
|
|
|
|
|
|
|
|
|
McDonnell XF-88 Voodoo
|
1949
|
 |
|
Aircraft on photo: McDonnell XF-88A Voodoo Photo source: USAF
|
|
Data for: XF-88A
|
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
1.130 km/h
|
(706 mph)
|
Length: |
Type:
|
escort fighter |
Combat range: |
NA
|
|
Span:
|
Description:
|
base design developed into F-101 Voodoo
|
Range:
|
2.779 km
|
(1.737 mi)
|
Height:
|
First flight:
|
1949 |
Ceiling: |
12.012 m |
(39.400 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
40 m/s
|
(8.000 ft/min)
|
Number built: |
|
16,50 m
|
(54 ft 1.5 in)
|
12,10 m
|
(39 ft 8 in)
|
5,30 m
|
(17 ft 3 in)
|
10.477 kg
|
(23.100 lb)
|
| 1 (2 |
total XF-88) |
|
| Engines: |
2 x Westinghouse J34 turbojets
|
|
|
Thrust:
|
2 x 21,4 kN (2 x 4.825 lbf)
|
|
|
Armament:
|
Guns: 6 x 20 mm (6 x 0.79 in) |
|
|
|
|
|
|
|
|
McDonnell XF-88B Voodoo
|
1953
|
 |
|
| Aircraft on photo: McDonnell XF-88B Voodoo Photo source: USAF |
|
| |
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
1,1 M
|
|
Length: |
Type:
|
experimental fighter |
Range: |
NA
|
|
Span:
|
Description:
|
first supersonic jet-turboprop hybrid
|
Ferry range:
|
NA
|
|
Height:
|
First flight:
|
1953
|
Ceiling: |
NA |
|
Max weight: |
Crew:
|
1
|
Rate of climb:
|
NA
|
|
Number built: |
|
17,68 m
|
(58 ft 0 in)
|
12,10 m
|
(39 ft 8 in)
|
5,30 m
|
(17 ft 3 in)
|
NA
|
|
| 1 (2 |
total XF-88) |
|
Engines:
|
2 x Westinghouse J34 turbojets
|
|
|
| |
1 x Alisson T38 turboprop
|
|
|
Thrust:
|
2 x 21,4 kN (2 x 4.825 lbf)
|
|
|
| Power: |
1 x 1.975 kW (1 x 2.650 HP) |
|
|
Armament:
|
NA |
|
|
|
|
|
|
|
|
McDonnell XF3H Demon
|
1951
|
 |
|
Aircraft on photo: McDonnell XF3H-1 Demon Photo source: US Navy
|
|
| |
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
NA
|
|
Length: |
Type:
|
carrier-based fighter aircraft
|
Range: |
NA
|
|
Span:
|
Description:
|
F3H Demon prototype
|
Ferry range:
|
NA
|
|
Height:
|
First flight:
|
1951
|
Ceiling: |
NA |
|
Max weight: |
Crew:
|
1
|
Rate of climb:
|
NA
|
|
Number built: |
|
18,08 m
|
(59 ft 4 in)
|
10,77 m
|
(35 ft 4 in)
|
4,45 m
|
(14 ft 7 in)
|
NA
|
|
2 prototypes
|
|
|
Engines:
|
1 x Westinghouse J40 turbojet
|
|
|
Thrust:
|
1 x 32 kN (1 x 7.200 lbf) dry thrust
|
|
|
|
1 x 48,4 kN (1 x 10.900 lbf) with afterburner
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
McDonnell F3H Demon
|
1951 |
 |
|
Aircraft on photo: McDonnell F3H-2 Demon Photo source: Flickr, Robert Sullivan
|
|
Data for: F3H-2
|
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
1.152 km/h
|
(716 mph)
|
Length: |
Type:
|
carrier-based fighter aircraft
|
Range: |
NA
|
|
Span:
|
Description:
|
XF3H with redesigned nose
|
Ferry range:
|
2.900 km
|
(1.800 mi)
|
Height:
|
First flight:
|
1951
|
Ceiling: |
13.000 m |
(42.650 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
72,9 m/s
|
(14.350 ft/min)
|
Number built: |
|
17,98 m
|
(59 ft 0 in)
|
10,77 m
|
(35 ft 4 in)
|
4,45 m
|
(14 ft 7 in)
|
17.700 kg
|
(39.000 lb)
|
519
|
(total F3H) |
|
| Engines: |
1 x Alisson J71 turbojet
|
|
|
Thrust:
|
1 x 63,39 kN (1 x 14.250 lbf) with afterburner
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
| |
Missiles: 4 x (Sparrow, Sidewinder)
|
|
|
| |
Bombs: 2.720 kg (6.000 lb)
|
|
|
|
|
|
|
|
|
McDonnell F-101 Voodoo
|
1954
|
 |
|
| Aircraft on photo: McDonnell F-101A Voodoo |
|
| Data for: F-101A |
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
1.720 km/h
|
(1.070 mph)
|
Length: |
Type:
|
strategic fighter aircraft
|
Range: |
1.275 km
|
(795 mi)
|
Span:
|
Description:
|
supersonic fighter developed from XF-88
|
Ferry range:
|
3.960 km
|
(2.460 mi)
|
Height:
|
First flight:
|
1954
|
Ceiling: |
17.010 m |
(55.800 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
224 m/s
|
(44.100 ft/min)
|
Number built: |
|
20,55 m
|
(67 ft 5 in)
|
12,09 m
|
(39 ft 8 in)
|
5,49 m
|
(18 ft 0 in)
|
22.260 kg
|
(49.070 lb)
|
807
|
(total F-101) |
|
| Engines: |
2 x Pratt & Whitney J57 turbojets
|
|
More info: |
Thrust:
|
2 x 45,4 kN (2 x 10.200 lbf) dry thrust
|
|
Airwar |
|
2 x 66,7 kN (2 x 15.000 lbf) with afterburner
|
|
National Museum |
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
Aero Web |
| |
Bombs: 3.050 kg (6.720 lb)
|
|
|
|
| Sources: |
| Rand McNally |
Encyclopedia
|
of Military Aircraft,
|
Enzo Angelucci, 1990
|
|
|
|
|
|
McDonnell F-101B/F Voodoo
|
1957
|
 |
|
| Aircraft on photo: McDonnell F-101B Voodoo Photo source: aircraftinformation.com |
|
Data for: F-101B
|
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
1.825 km/h
|
(1.134 mph)
|
Length: |
Type:
|
two-seat interceptor
|
Range: |
2.450 km
|
(1.520 mi)
|
Span:
|
Description:
|
more powerful engines w. long afterburner
|
Ferry range:
|
3.106 km
|
(1.930 mi)
|
Height:
|
First flight:
|
1957
|
Ceiling: |
17.800 m |
(58.400 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
250 m/s
|
(49.200 ft/min)
|
Number built: |
|
20,55 m
|
(67 ft 5 in)
|
12,09 m
|
(39 ft 8 in)
|
5,49 m
|
(18 ft 0 in)
|
23.770 kg
|
(52.400 lb)
|
479
|
(total 807) |
|
| Engines: |
2 x Pratt & Whitney J57 turbojets
|
|
|
Thrust:
|
2 x 53,3 kN (2 x 11.990 lbf) dry thrust
|
|
|
|
2 x 75,2 kN (2 x 16.900 lbf) with afterburner
|
|
|
| Armament: |
4 x missiles
|
|
|
|
|
|
|
|
|
McDonnell F3H-G (mock up)
|
1955
|
 |
|
| Aircraft on photo: McDonnell F3H-G Photo source: vectorsite.net |
|
Data for: F3H-G
|
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
1,52 M
|
|
Length: |
Type:
|
carrier-based fighter aircraft
|
Range: |
NA
|
|
Span:
|
Description:
|
twin-engined Demon adaptation & basis for Phantom II
|
Ferry range:
|
NA
|
|
Height:
|
Cancelled:
|
1955
|
Ceiling: |
NA |
|
Max weight: |
Crew:
|
1
|
Rate of climb:
|
NA
|
|
Number built: |
|
17,07 m
|
(56 ft 0 in)
|
12,14 m
|
(39 ft 9 in)
|
5,18 m
|
(17 ft 0 in)
|
NA
|
|
1 mock up
|
|
|
| Engines: |
2 x Wright J65 turbojets
|
|
|
Thrust:
|
2 x 34,59 kN (2 x 7.800 lbf) |
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
|
Hardpoints: 9 |
|
|
|
|
|
|
|
|
McDonnell XF4H-1
|
1958 |
 |
|
| Aircraft on photo: McDonnell XF4H-1 Photo source: tailspintopics.blogspot.com |
|
Data for: XF4H-1
|
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
2.585 km/h
|
(1.606 mph)
|
Length: |
Type:
|
fighter bomber
|
Combat range: |
NA
|
|
Span:
|
Description:
|
F-4 Phantom II prototype with small nose
|
Ferry range:
|
NA
|
|
Height:
|
First flight:
|
1958
|
Ceiling: |
30.048 m |
(98.557 ft) |
Max weight: |
Crew:
|
2
|
Rate of climb:
|
9.000 ft in 34,5
|
sec (2.743 m) |
Number built: |
|
17,3 m
|
(56 ft 10 in)
|
11,6 m
|
(38 ft 4 in)
|
4,9 m
|
(16 ft 3 in)
|
NA
|
|
2 (XF4H-1),
|
5 (YF4H-1)
|
|
| Engines: |
2 x General Electric J79 turbojets
|
|
|
|
2 x 46 kN (2 x 10.350 lbf) dry thrust
|
|
|
| Thrust: |
2 x 70,95 kN (2 x 16.000 lbf) with afterburner
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
McDonnell F-4 Phantom II
|
1958 |
 |
|
| Aircraft on photo: McDonnell F-4D Phantom II Photo source: richard-seaman.com |
|
Data for: F-4B
|
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
2.548 km/h
|
(1.583 mph)
|
Length: |
Type:
|
fighter bomber
|
Combat range: |
800 km
|
(500 mi)
|
Span:
|
Description:
|
principal USAF&USN air superiority fighter
|
Ferry range:
|
2.592 km
|
(1.610 mi)
|
Height:
|
First flight:
|
1958
|
Ceiling: |
18.900 m |
(62.000 ft) |
Max weight: |
Crew:
|
2
|
Rate of climb:
|
207 m/s
|
(40.800 ft/min)
|
Number built: |
|
17,76 m
|
(58 ft 3 in)
|
11,70 m
|
(38 ft 5 in)
|
4,96 m
|
(16 ft 3 in)
|
24.766 kg
|
(54.600 lb)
|
5.195
|
|
|
| Engines: |
2 x General Electric J79 turbojets
|
|
|
Thrust:
|
2 x 70,95 kN (2 x 16.000 lbf)
|
|
|
| Armament: |
Bombs: 7.257 kg (16.000 lb)
|
|
|
|
Missiles: 8 x air-to-air
|
|
|
|
|
|
|
|
|
McDonnell F-4J / K / M Phantom II
|
1965 |
 |
|
| Aircraft on photo: McDonnell F-4K Phantom II Photo source: Wikipedia |
|
Data for: F-4J
|
|
Manufacturer:
|
McDonnell Aircraft, USA |
Max speed:
|
2.389 km/h
|
(1.485 mph)
|
Length: |
Type:
|
fighter-bomber |
Range: |
1.450 km
|
(900 mi)
|
Span:
|
Description:
|
F4 without infrared seeker under nose |
Ferry range:
|
3.150 km
|
(1.956 mi)
|
Height:
|
First flight:
|
1965
|
Ceiling: |
18.900 m |
(62.000 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
209,5 m/s
|
(41.250 ft/min)
|
Number built: |
|
17,76 m
|
(58 ft 3 in)
|
11,70 m
|
(38 ft 5 in)
|
4,96 m
|
(16 ft 3 in)
|
25.396 kg
|
(56.000 lb)
|
522 (F-4J),
|
50 (F-4K),
|
|
| Engines: |
2 x General Electric J79 turbojets
|
|
|
Thrust:
|
2 x 79,55 kN (2 x 17.900 lbf)
|
More info / sources:
|
Aero Web
|
| Armament: |
Bombs and missiles: 7.257 kg (16.000 lb)
|
Global Security |
F-4J at f-4.nl
|
|
|
|
|
|
|
McDonnell Douglas F-4E / F Phantom II
|
1967
|
 |
|
Aircraft on photo: McDonnell F-4F Phantom II
|
|
Data for F-4E
|
|
Manufacturer:
|
McDonnell Douglas, USA |
Max speed:
|
2.513 km/h
|
(1.500 mph)
|
Length: |
Type:
|
fighter-bomber |
Combat range: |
800 km
|
(500 mi)
|
Span:
|
Description:
|
leading Phantom II model with longer nose
|
Ferry range:
|
2.600 km
|
(1.615 mi)
|
Height:
|
First flight:
|
1967
|
Ceiling: |
19.000 m |
(62.340 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
210 m/s
|
(41.300 ft/min)
|
Number built: |
|
19,20 m
|
(63 ft 0 in)
|
11,70 m
|
(38 ft 5 in)
|
4,96 m
|
(16 ft 3 in)
|
28.030 kg
|
(61.795 lb)
|
1389 (F-4E)
|
,175 (F-4F) |
|
| Engines: |
2 x General Electric J79 turbojets
|
|
|
Thrust:
|
2 x 79,55 kN (2 x 17.900 lbf)
|
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in)
|
|
|
|
Bombs: 7.257 kg (16.000 lb)
|
|
|
|
|
|
|
|
|
McDonnell Douglas YF-4E CCV
|
1974 |
 |
|
Aircraft on photo: McDonnell YF-4E CCV Photo source: Avia Deja Vu
|
|
| |
|
Manufacturer:
|
McDonnell Douglas, USA |
Max speed:
|
2.334 km/h
|
(1.450 mph)
|
Length: |
Type:
|
experimental fighter |
Combat range: |
NA
|
|
Span:
|
Description:
|
Control Configured Vehicle (CCV) testbed
|
Ferry range:
|
NA
|
|
Height:
|
First flight:
|
1974
|
Ceiling: |
18.166 m |
(59.600 ft) |
Max weight: |
Crew:
|
2
|
Rate of climb:
|
NA
|
|
Number built: |
|
19,20 m
|
(63 ft 0 in)
|
11,70 m
|
(38 ft 5 in)
|
5,03 m
|
(16 ft 6 in)
|
26.308 kg
|
(58.000 lb)
|
1
|
|
|
| Engines: |
2 x General Electric J79 turbojets
|
|
More info / sources: |
Thrust:
|
2 x 79,55 kN (2 x 17.900 lbf)
|
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in)
|
|
|
|
Ordnance: 7.257 kg (16.000 lb)
|
|
|
|
|
|
|
|
|
McDonnell Douglas F-15 Eagle
|
1972
|
 |
|
Aircraft on photo: McDonnell Douglas F-15C Eagle
|
|
Data for: F-15C
|
|
Manufacturer:
|
McDonnell Douglas, USA |
Max speed:
|
2.660 km/h
|
(1.650 mph)
|
Length: |
Type:
|
air superiority fighter |
Combat range: |
1.967 km
|
(1.222 mi)
|
Span:
|
Description:
|
twin-engine all weather tactical fighter
|
Ferry range:
|
5.550 km
|
(3.450 mi)
|
Height:
|
First flight:
|
1972
|
Ceiling: |
20.000 m |
(65.000 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
254 m/s
|
(50.000 ft/min)
|
Number built: |
|
19,43 m
|
(63 ft 9 in)
|
13,05 m
|
(42 ft 10 in)
|
5,63 m
|
(18 ft 6 in)
|
30.845 kg
|
(68.000 lb)
|
1.533+
|
(total F-15) |
|
| Engines: |
2 x Pratt & Whitney F100 afterburning turbofans
|
|
|
Thrust:
|
2 x 77,62 kN (2 x 17.450 lbf) dry thrust
|
|
|
|
2 x 111,2 kN (2 x 25.000 lbf) with afterburner
|
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
Hardpoints: 11 |
|
|
| |
Hardpoints capacity: 7.300 kg (16.000 lbf)
|
|
|
|
|
|
|
|
|
McDonnell Douglas F-15B / D Eagle
|
1973
|
 |
|
Aircraft on photo: McDonnell Douglas F-15D Eagle
|
|
Data for: F-15D
|
|
Manufacturer:
|
McDonnell Douglas, USA |
Max speed:
|
2.657 km/h
|
(1.650 mph)
|
Length: |
Type:
|
air superiority fighter
|
Combat range: |
NA
|
|
Span:
|
Description:
|
fully combat capable 2-seat training version
|
Ferry range:
|
4.637 km
|
(2.880 mi)
|
Height:
|
First flight:
|
1973
|
Ceiling: |
18.897 m |
(62.000 ft) |
Max weight: |
Crew:
|
2
|
Rate of climb:
|
254 m/s
|
(50.000 ft/min)
|
Number built: |
|
19,43 m
|
(63 ft 9 in)
|
13,00 m
|
(42 ft 9 in)
|
5,63 m
|
(18 ft 6 in)
|
30.845 kg
|
(68.000 lb)
|
61 (F-15B),
|
92 (F-15D),
|
|
| Engines: |
2 x Pratt & Whitney F100 afterburning turbofans |
|
|
Thrust:
|
2 x 66 kN (2 x 14.870 lbf) dry thrust
|
|
|
|
2 x 106 kN (2 x 23.830 lbf) with afterburner
|
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
Hardpoints: 11 |
|
|
| |
Hardpoints capacity: NA |
|
|
|
|
|
|
|
|
McDonnell Douglas F-15E Strike Eagle
|
1986 |
 |
|
| Aircraft on photo: McDonnell Douglas F-15E Strike Eagle Photo source: Wikipedia |
|
| Data for: F-15E |
|
Manufacturer:
|
McDonnell Douglas, USA |
Max speed:
|
2.650 km/h
|
(1.650 mph)
|
Length: |
Type:
|
all-weather ground attack strike fighter
|
Range: |
NA
|
|
Span:
|
Description:
|
deep strikes & close air support 2 seat F-15
|
Ferry range:
|
3.900 km
|
(2.400 mi)
|
Height:
|
First flight:
|
1986
|
Ceiling: |
18.200 m |
(60.000 ft |
Max weight: |
Crew:
|
2
|
Rate of climb:
|
254 m/s
|
(50.000 ft/min)
|
Number built: |
|
19,43 m
|
(63 ft 9 in)
|
13,00 m
|
(42 ft 9 in)
|
5,63 m
|
(18 ft 6 in)
|
36.700 kg
|
(81.000 lb)
|
334+
|
|
|
| Engines: |
2 x Pratt & Whitney F100 afterburning turbofans |
|
|
Thrust:
|
2 x 79,18 kN (2 x 17.800 lbf) dry thrust
|
|
|
|
2 x 129,45 kN (2 x 29.100 lbf) with afterburner
|
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
Hardpoints capacity: 11.000 kg (24.250 lb)
|
|
|
|
|
|
|
|
|
McDonnell Douglas F-15 Active
|
1988 |
 |
|
Aircraft on photo: McDonnell Douglas F-15 Active
|
|
Data for: F-15 Active
|
|
Manufacturer:
|
McDonnell Douglas, USA |
Max speed:
|
2.645 km/h
|
(1.643 mph)
|
Length*: |
Type:
|
technology demonstrator
|
Range: |
NA
|
|
Span:
|
Description:
|
canard foreplanes and thrust-vectoring F-15
|
Ferry range:
|
NA
|
|
Height:
|
First flight:
|
1988
|
Ceiling: |
18.288 m |
(60.000 ft) |
Max weight: |
Crew:
|
2
|
Rate of climb:
|
NA
|
|
Number built: |
|
19,42 m
|
(63.7 ft)
|
13,00 m
|
(42.8 ft)
|
5,64 m
|
(18.47 ft)
|
NA
|
|
1
|
|
|
| Engines: |
2 x Pratt & Whitney F100 afterburning turbofan |
|
*(without nose boom) |
Thrust:
|
2 x 104 kN (2 x 23.450 lbf) dry thrust
|
|
|
|
2 x 129 kN (2 x 29.000 lbf) with afterburner
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Boeing F-15SE Silent Eagle
|
2010
|
 |
|
| Aircraft on photo: Boeing F-15SE Silent Eagle Photo source: Boeing |
|
Data for: F-15SE mock up
|
|
Manufacturer:
|
Boeing IDS, USA |
Max speed:
|
2.655 km/h
|
(1.650 mph)
|
Length: |
Type:
|
multi-role fighter |
Range: |
NA
|
|
Span:
|
Description:
|
F-15 stealth upgrade with internal weapons |
Ferry range:
|
3.900 km
|
(2.423 mi)
|
Height:
|
| |
bays and radar absorbent materials
|
Ceiling: |
18.200 m |
(59.711 ft) |
Max weight: |
First flight:
|
2010
|
Rate of climb: |
254 m/s
|
(50.000 ft/min)
|
Number built: |
Crew:
|
2
|
|
|
|
|
|
19,43 m
|
(63.75 ft)
|
13,05 m
|
(42.81 ft)
|
5,63 m
|
(18.47 ft)
|
36.700 kg
|
(80.910 lb)
|
1
|
|
| |
|
|
| Engines: |
2 x Pratt & Whitney F100 afterburning turbofan |
|
|
Thrust:
|
2 x 79,18 kN (2 x 17.800 lbf) dry thrust
|
|
|
|
2 x 129,45 kN (2 x 29.100 lbf) with afterburner
|
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
External hardpoints and 4 x internal weapons bays |
|
|
|
|
|
|
|
|
McDonnell Douglas F/A-18 Hornet
|
1978
|
 |
|
| Aircraft on photo: McDonnell Douglas F/A-18C Hornet |
|
| Data for: F/A-18C |
|
Manufacturer:
|
McDonnell Douglas, USA |
Max speed:
|
1.915 km/h
|
(1.190 mph)
|
Length: |
Type:
|
multi-role fighter |
Range: |
740 km
|
(460 mi)
|
Span:
|
Description:
|
designed for dogfight and ground attack |
Ferry range:
|
3.335 km
|
(2.070 mi)
|
Height:
|
First flight:
|
1978
|
Ceiling: |
15.240 m |
(50.000 ft |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
229 m/s
|
(45.000 ft/min) |
Number built: |
|
17,07 m
|
(56 ft 0 in)
|
11,43 m
|
(37 ft 6 in)
|
4,66 m
|
(15 ft 4 in)
|
25.400 kg
|
(56.000 lb)
|
1.480
|
(F/A-18A-D) |
|
| Engines: |
2 x General Electric F404 turbofans |
|
|
Thrust:
|
2 x 48,9 kN (2 x 11.000 lbf) dry thrust
|
|
|
|
2 x 78,7 kN (2 x 17.700 lbf) with afterburner
|
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
Hardpoints: 9 (2 at wingtips, 4 under wings, 3 under fuselage) |
|
|
| |
Ordnance: 7.030 kg (15.500 lb) of rockets, bombs and missiles
|
|
|
|
|
|
|
|
|
McDonnell Douglas F/A-18B / D Hornet
|
1979
|
 |
|
| Aircraft on photo: McDonnell Douglas F/A-18B Hornet |
|
| Data for: F/A-18D |
|
Manufacturer:
|
McDonnell Douglas, USA |
Max speed:
|
1.916 km/h
|
(1.190 mph)
|
Length: |
Type:
|
fighter-trainer aircraft
|
Range: |
NA
|
|
Span:
|
Description:
|
fully combat capable F-18 trainer version
|
Ferry range:
|
NA
|
|
Height:
|
First flight:
|
1979 (F/A-18B)
|
Ceiling: |
15.239 m |
(50.000 ft) |
Max weight: |
Crew:
|
2
|
Rate of climb:
|
229 m/s
|
(45.000 ft/min)
|
Number built: |
|
17,07 m
|
(56 ft 0 in)
|
11,43 m
|
(37 ft 6 in)
|
4,66 m
|
(15 ft 4 in)
|
25.400 kg
|
(56.000 lb)
|
1.480
|
(F/A-18A-D) |
|
| Engines: |
2 x General Electric F404 turbofans |
|
|
Thrust:
|
2 x 48,9 kN (2 x 11.000 lbf) dry thrust |
|
|
|
2 x 78,7 kN (2 x 17.700 lbf) with afterburner |
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
Hardpoints: 9 (2 at wingtips, 4 under wings, 3 under fuselage) |
|
|
| |
Ordnance: 7.030 kg (15.500 lb) of rockets, bombs and missiles |
|
|
|
|
|
|
|
|
Boeing F/A-18E Super Hornet
|
1995
|
 |
|
Aircraft on photo: Boeing F/A-18E Super Hornet
|
|
| Data for: F/A-18E |
|
Manufacturer:
|
Boeing IDS, USA |
Max speed:
|
1.915 km/h
|
(1.190 mph)
|
Length: |
Type:
|
multi-role fighter |
Combat range: |
760 km
|
(475 mi)
|
Span:
|
Description:
|
Hornet larger and more advanced derivative
|
Ferry range:
|
3.330 km
|
(2.070 mi)
|
Height:
|
First flight:
|
1995
|
Ceiling: |
15.239 m |
(50.000 ft) |
Max weight: |
Crew:
|
1
|
Rate of climb:
|
NA
|
|
Number built: |
|
18,31 m
|
(60 ft 1 in)
|
13,62 m
|
(44 ft 9 in)
|
4,88 m
|
(16 ft 0 in)
|
29.937 kg
|
(66.000 lb)
|
+400
|
(F/A-18E&F) |
|
| Engines: |
2 x General Electric F414 turbofans |
|
More info / sources: |
Thrust:
|
2 x 62,3 kN (2 x 14.000 lbf) dry thrust
|
|
|
|
2 x 97,9 kN (2 x 22.000 lbf) with afterburner
|
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
Hardpoints: 11 (2 at wingtips, 6 under wings, 3 under fuselage) |
|
|
| |
Ordnance: 8.050 kg (17.750 lb) of rockets, bombs and missiles |
|
|
|
|
|
|
|
|
Boeing F/A-18F Super Hornet
|
1996
|
 |
|
| Aircraft on photo: Boeing F/A-18F Super Hornet |
|
| Data for: F/A-18F |
|
Manufacturer:
|
Boeing IDS, USA |
Max speed:
|
1.960 km/h
|
(1.218 mph)
|
Length: |
Type:
|
multi-role fighter |
Range: |
740 km
|
(460 mi)
|
Span:
|
Description:
|
tandem seat F/A-18E variant
|
Ferry range:
|
2.700 km
|
(1.678 mi)
|
Height:
|
First flight:
|
1996
|
Ceiling: |
15.239 m |
(50.000 ft) |
Max weight: |
Crew:
|
2
|
Rate of climb:
|
NA
|
|
Number built: |
|
18,31 m
|
(60 ft 1 in)
|
13,62 m
|
(44 ft 9 in)
|
4,88 m
|
(16 ft 0 in)
|
29.937 kg
|
(66.000 lb)
|
+400
|
(F/A-18E&F) |
|
| Engines: |
2 x General Electric F414 turbofans |
|
|
Thrust:
|
2 x 62,3 kN (2 x 14.000 lbf) dry thrust |
|
|
|
2 x 97,9 kN (2 x 22.000 lbf) with afterburner |
|
|
| Armament: |
Gun: 1 x 20 mm (1 x 0.79 in) |
|
|
| |
Hardpoints: 11 (2 at wingtips, 6 under wings, 3 under fuselage) |
|
|
| |
Ordnance: 8.050 kg (17.750 lb) of rockets, bombs and missiles |
|
|
|
|
|
|
|
| |
|
