|
Avro 720
|
1957 |
|
–Avro –Blackburn–Folland-
|
Aircraft on photo: Avro 720 Photo source: Defence.pk
|
|
| |
|
Manufacturer:
|
Avro Aircraft, United Kingdom
|
Max speed:
|
2.120 km/h
|
(1.320 mph) |
Length: |
Type:
|
interceptor prototype
|
Range: |
NA
|
|
Span:
|
Description:
|
mixed propulsion interceptor with a rocket |
Ferry range:
|
NA
|
|
Height:
|
| |
engine to give high performance and a
|
Ceiling: |
18.288 m
|
(60.000 ft)
|
Max weight: |
| |
small jet engine for cruising flight |
Climb rate: |
110,9 m/s |
(21.820 ft/min)
|
Number built: |
Canceled:
|
1956
|
Crew: |
1 |
|
|
|
12,88 m
|
(42 ft 3 in)
|
8,32 m
|
(27 ft 4 in)
|
NA
|
|
7.972 kg
|
(17.575 lb)
|
| 1 uncompleted |
prototype |
| |
|
|
| Engines: |
1 × Armstrong Siddeley Screamer liquid-fuelled rocket
|
|
|
| |
1 × Armstrong Siddeley Viper ASV.8 turbojet
|
|
|
| Thrust: |
1 x 36 kN (1 x 8.000 lbf) rocket engine
|
|
|
| |
1 x 7,8 kN (1 x 1.750 lbf) turbojet |
|
|
| Armament: |
Missiles: provision for 2 x air-to-air missiles
|
|
|
|
|
| |
|
|
Blackburn B-48 Firecrest
|
1947
|
|
|
Aircraft on photo: Blackburn B-48 Firecrest Photo source: Flickr by kitchener.lord
|
|
| |
|
Manufacturer:
|
Blackburn Aircraft, United Kingdom
|
Max speed:
|
612 km/h
|
(380 mph) |
Length: |
Type:
|
strike fighter
|
Range: |
1.450 km
|
(900 mi)
|
Span:
|
Description:
|
single-engine naval strike fighter built as |
Ferry range:
|
2.315 km
|
(1.438 mi)
|
Height:
|
| |
B-35 Firebrand development |
Ceiling: |
10.210 m
|
(33.497 ft)
|
Max weight: |
| First flight: |
1947
|
Climb rate: |
12,7 m/s
|
(2.500 ft/min)
|
Number built: |
| Crew: |
1
|
|
|
|
|
|
11,98 m
|
(39 ft 4 in)
|
13,71 m
|
(45 ft 0 in)
|
4,42 m
|
(14 ft 6 in)
|
6.887 kg
|
(15.183 lb)
|
| 3 |
|
| |
|
|
| Engine: |
1 × Bristol Centaurus 59 18-cylinder radial engine
|
|
|
| Power: |
1 x 1.846 kW (1 x 2.475 HP)
|
|
|
| Armament: |
Guns: 2 x 12,7 mm (2 x 0.50 in)
|
|
|
| |
Rockets: 8 on underwing rails
|
|
|
| |
Torpedo / bombs: 1 x 951 kg (2.097 lb) torpedo or 2 x 110 kg (250 lb) bombs
|
|
|
|
|
|
|
|
|
De Havilland D.H.100 Vampire
|
1943 |
|
|
Aircraft on photo: De Havilland (FFA) D.H.100 Vampire FB6
|
|
| Data for: De Havilland D.H.100 Vampire FB6 |
|
Manufacturer:
|
de Havilland Aircraft Company, United Kingdom
|
Max speed:
|
882 km/h
|
(548 mph) |
Length: |
Type:
|
fighter aircraft
|
Range: |
1.960 km
|
(1.220 mi)
|
Span:
|
Description:
|
second jet fighter in RAF service after Meteor |
Ferry range:
|
2.253 km
|
(1.400 mi)
|
Height:
|
| First flight: |
1943 |
Ceiling: |
13.045 m
|
(42.800 ft)
|
Max weight: |
| Crew: |
1 |
Climb rate: |
24,4 m/s
|
(4.800 ft/min)
|
Number built: |
|
9,37 m
|
(30 ft 9 in)
|
11,58 m
|
(38 ft 0 in)
|
2,69 m
|
(8 ft 10 in)
|
5.620 kg
|
(12.390 lb)
|
3.268
|
(total) |
|
| Engine: |
1 × de Havilland Goblin 3 centrifugal turbojet
|
|
More info/sources: |
| Thrust: |
1 x 14,90 kN (1 x 3.350 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
| |
Rockets: 8 |
|
|
| |
Bombs: 2 x 225 kg (2 x 500 lb) |
|
|
|
|
|
|
|
|
De Havilland D.H.115 Vampire
|
1951 |
|
|
| Aircraft on photo: De Havilland D.H.115 Vampire T55 |
|
| Data for: De Havilland D.H.115 Vampire T11 |
|
Manufacturer:
|
de Havilland Aircraft Company, United Kingdom
|
Max speed:
|
885 km/h
|
(550 mph) |
Length: |
Type:
|
fighter-trainer
|
Range: |
1.370 km
|
(851 mi)
|
Span:
|
Description:
|
D.H.100 two-seat training version |
Ferry range:
|
NA
|
|
Height:
|
| First flight: |
1950 |
Ceiling: |
12.200 m
|
(40.026 ft)
|
Max weight: |
| Crew: |
2 |
Climb rate: |
NA
|
|
Number built: |
|
10,55 m
|
(34 ft 7 in)
|
11,58 m
|
(38 ft 0 in)
|
1,90 m
|
(6 ft 3 in)
|
5.960 kg
|
(13.140 lb)
|
1.130
|
(trainers) |
|
| Engine: |
1 × de Havilland Goblin 35 centrifugal turbojet
|
|
|
|
| (T.11 / 22 / 33 / 34 / 35 / 55) |
|
Thrust:
|
1 x 15,59 kN (1 x 3.505 lbf)
|
|
More info/sources:
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
|
|
|
|
|
|
De Havilland D.H.112 Venom
|
1949
|
|
|
Aircraft on photo: De Havilland D.H.112 Venom FB50 (long nose)
|
|
| Data for: De Havilland D.H.112 Venom FB1 |
|
Manufacturer:
|
de Havilland Aircraft Comp., United Kingdom
|
Max speed:
|
1.030 km/h
|
(640 mph) |
Length: |
Type:
|
fighter-bomber
|
Range: |
1.730 km
|
(1.080 mi)
|
Span:
|
Description:
|
British postwar single-engined jet aircraft |
Fer. range:
|
NA
|
|
Height:
|
| |
developed from de Havilland Vampire
|
Ceiling: |
13.720 m
|
(45.013 ft)
|
Loaded weight: |
| |
and designed for Ghost engine |
Climb rate: |
45,7 m/s |
(9.000 ft/min)
|
Number built: |
First flight:
|
1949
|
Crew: |
1 |
|
|
|
9,70 m
|
(31 ft 10 in)
|
12,70 m
|
(41 ft 8 in)
|
1,88 m
|
(6 ft 2 in)
|
7.000 kg
|
(15.400 lb)
|
663
|
(fighter-bombers: |
| FB1 / FB |
4 / FB50 / FB54)
|
|
| Engine: |
1 × de Havilland Ghost 103 turbojet
|
|
|
| Thrust: |
1 x 21,6 kN (1 x 4.850 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
| |
Rockets: 8 |
|
|
| |
Bombs: 2 x 454 kg (2 x 1.000 lb) |
|
|
|
|
|
|
|
|
De Havilland DH.112 Venom NF
|
1950
|
|
|
| Aircraft on photo: De Havilland D.H.112 Venom NF2 |
|
| Data for: De Havilland D.H.112 Venom NF2 |
|
Manufacturer:
|
de Havilland Aircraft Company, United Kingdom
|
Max speed:
|
1.013 km/h
|
(630 mph) |
Length: |
Type:
|
night fighter
|
Range: |
1.600 km
|
(995 mi)
|
Span:
|
Description:
|
Venom two-seat night fighter version |
Ferry range:
|
NA
|
|
Height:
|
| First flight: |
1950 |
Ceiling: |
15.000 m
|
(49.212 ft)
|
Loaded weight: |
| Crew: |
2 |
Climb rate: |
NA
|
|
Number built: |
|
11,17 m
|
(36 ft 8 in)
|
12,70 m
|
(41 ft 8 in)
|
2,00 m
|
(6 ft 7 in)
|
7.166 kg
|
(15.800 lb)
|
| 274 |
(night fighters) |
|
| Engine: |
1 × de Havilland Ghost 104 turbojet
|
|
More info/sources: |
| Thrust: |
1 x 22 kN (1 x 4.950 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
|
|
|
|
|
|
De Havilland DH-112 Sea Venom
|
1951 |
|
|
| Aircraft on photo: De Havilland D.H.112 Sea Venom FAW22 |
|
| Data for: De Havilland D.H.112 Sea Venom FAW22 |
|
Manufacturer:
|
de Havilland Aircraft Company, United Kingdom
|
Max speed:
|
927 km/h
|
(575 mph) |
Length: |
Type:
|
naval fighter-bomber
|
Range: |
1.135 km
|
(705 mi)
|
Span:
|
Description:
|
carrier-capable Venom version used in UK, |
Fer. range:
|
NA
|
|
Height:
|
| |
Australia and France (as SNCASE Aquilon) |
Ceiling: |
12.040 m
|
(39.500 ft)
|
Max weight: |
| First flight: |
1951 |
Climb rate: |
29,2 m/s |
(5.750 ft/min)
|
Number built: |
| Crew: |
2 |
|
|
|
|
|
11,15 m
|
(36 ft 7 in)
|
13,06 m
|
(42 ft 10 in)
|
2,60 m
|
(8 ft 6 in)
|
7.167 kg
|
(15.800 lb)
|
| 296 |
(Sea Venoms) |
| 90 |
(Aquilons) |
|
| Engine: |
1 × de Havilland Ghost 105 turbojet
|
|
|
| Thrust: |
1 x 23,6 kN (1 x 5.300 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
| |
Rockets: 8 |
|
|
| |
Bombs: 2 x 454 kg (2 x 1.000 lb) |
|
|
|
|
|
|
|
|
De Havilland DH-110
|
1951 |
 |
|
Aircraft on photo: De Havilland D.H.110 P1 (WG236) Photo source: Avia Deja Vu
|
|
| Data for: De Havilland D.H.110 P2 (WG240) |
|
Manufacturer:
|
de Havilland Aircraft Company, United Kingdom
|
Max speed:
|
1.110 km/h
|
(690 mph) |
Length: |
Type:
|
fighter prototype
|
Range: |
NA
|
|
Span:
|
Description:
|
unarmed prototypes of future Sea Vixen |
Ferry range:
|
NA
|
|
Height:
|
| First flight: |
1951 |
Ceiling: |
15.000 m
|
(49.213 ft)
|
Max weight: |
| Crew: |
2 |
Climb rate: |
NA
|
|
Number built: |
|
15,75 m
|
(51 ft 8 in)
|
15,54 m
|
(51 ft 0 in)
|
3,35 m
|
(11 ft 0 in)
|
15.875 kg
|
(35.000 lb)
|
| 3 |
prototypes |
|
| Engines: |
2 × Rolls-Royce Avon RA.7 turbojets
|
|
More info/sources: |
| Thrust: |
2 x 33,36 kN (2 x 7.500 lbf)
|
|
|
| Armament: |
None
|
|
|
|
|
|
|
|
|
Hawker Siddeley DH-110 Sea Vixen
|
1951
|
|
|
| Aircraft on photo: Hawker Siddeley D.H.110 Sea Vixen D.3 |
|
| Data for: Hawker Siddeley D.H.110 Sea Vixen FAW2 |
|
Manufacturer:
|
Hawker Siddeley Aviation, United Kingdom
|
Max speed:
|
1.110 km/h
|
(690 mph) |
Length: |
Type:
|
carrier-based fighter
|
Range: |
1.270 km
|
(790 mi)
|
Span:
|
Description:
|
second generation carrier capable jet fighter |
Ferry range:
|
1.480 km
|
(920 mi)
|
Height:
|
| First flight: |
1951 (D.H.110), 1955 (Sea Vixen) |
Ceiling: |
15.000 m
|
(48.000 ft)
|
Max weight: |
| Crew: |
2 |
Climb rate: |
46 m/s
|
(9.000 ft/min)
|
Number built: |
|
16,94 m
|
(55 ft 7 in)
|
15,54 m
|
(51 ft 0 in)
|
3,28 m
|
(10 ft 9 in)
|
21.205 kg
|
(46.750 lb)
|
| 145 |
(total) |
|
| Engines: |
2 × Rolls-Royce Avon Mk.208 turbojets
|
|
|
| Thrust: |
2 x 50 kN (2 x 11.000 lbf)
|
|
|
| Armament: |
Hardpoints: 6 (4 rockets, 4 missiles or 2 x 227 kg (2 x 500 lb) bombs)
|
|
|
|
|
|
|
|
|
English Electric P1A
|
1954 |
 |
|
Aircraft on photo: English Electric P.1A
|
|
| Data for: English Electric P.1A |
|
Manufacturer:
|
English Electric, United Kingdom
|
Max speed:
|
1,53 Mach
|
|
Length: |
Type:
|
interceptor prototype
|
Range: |
NA
|
|
Span:
|
Description:
|
Lightning prototype with twin engines fed |
Ferry range:
|
NA
|
|
Height:
|
| |
by a single nose inlet, first British aircraft to
|
Ceiling: |
NA
|
|
Max weight: |
| |
exceed Mach 1 in level flight |
Climb rate: |
NA |
|
Number built: |
First flight:
|
1954
|
Crew: |
1 |
More |
info/sources: |
|
|
| Engines: |
2 × Armstrong Siddeley Sapphire turbojets
|
|
|
| Thrust: |
2 x 36 kN (2 x 8.100 lbf)
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
English Electric / BAC Lightning
|
1957
|
|
|
Aircraft on photo: BAC Lightning F.3
|
|
| Data for: BAC Lightning F.6 |
|
Manufacturer:
|
English Electric, United Kingdom
|
Max speed:
|
2.415 km/h
|
(1.500 mph) |
Length: |
Type:
|
interceptor
|
Range: |
1.370 km
|
(850 mi)
|
Span:
|
Description:
|
the only all-British Mach 2 fighter aircraft |
Ferry range:
|
2.040 km
|
(1.270 mi)
|
Height:
|
| |
with vertically stacked, longitudinally
|
Ceiling: |
18.300 m
|
(60.400 ft)
|
Max weight: |
| |
staggered engines |
Climb rate: |
254 m/s |
(50.000 ft/min)
|
Number built: |
| First flight: |
1957 (English Electric P.1B) |
Crew: |
1 |
|
|
|
16,8 m
|
(55 ft 3 in)
|
10,6 m
|
(34 ft 10 in)
|
5,97 m
|
(19 ft 7 in)
|
21.800 kg
|
(48.060 lb)
|
| 337 |
(total) |
| |
|
|
| Engines: |
2 × Rolls-Royce Avon 301R afterburning turbojets
|
|
|
| Thrust: |
2 x 55,74 kN (2 x 12.530 lbf) dry thrust
|
|
|
| |
2 x 71,17 kN (2 x 16.000 lbf) with afterburner
|
|
|
| Armament: |
Guns: 2 x 30 mm (2 x 1.18 in)
|
|
|
| |
Hardpoints: 2 under fuselage and 2 overwing
|
|
|
|
|
|
|
|
|
English Electric / BAC Lightning T
|
1959
|
|
|
| Aircraft on photo: BAC Lightning T.5 Photo source: Flickr by Steve Crane |
|
| Data for: BAC Lightning T.4 |
|
Manufacturer:
|
English Electric, United Kingdom
|
Max speed:
|
2.120 km/h
|
(1.300 mph) |
Length: |
Type:
|
interceptor-trainer
|
Range: |
1.120 km
|
(1.373 mi)
|
Span:
|
Description:
|
Lightning 2-seat side-by-side training version |
Ferry range:
|
NA
|
|
Height:
|
| First flight: |
1959 |
Ceiling: |
18.300 m
|
(60.400 ft)
|
Max weight: |
| Crew: |
2 |
Climb rate: |
254 m/s
|
(50.000 ft/min)
|
Number built: |
|
16,84 m
|
(55 ft 3 in)
|
10,56 m
|
(34 ft 8 in)
|
5,97 m
|
(19 ft 7 in)
|
22.000 kg
|
(48.500 lb)
|
| 52 |
(trainers) |
|
| Engines: |
2 × Rolls-Royce Avon 301P afterburning turbojets
|
|
More info/sources: |
| Thrust: |
2 x 60 kN (2 x 13.490 lbf) dry thrust
|
|
|
| |
2 x 72,76 kN (2 x 16.358 lbf) with afterburner
|
|
|
| Armament: |
Hardpoints: 2 under fuselage and 2 overwing
|
|
|
| |
|
|
|
|
|
|
|
|
|
Folland Fo-139 Midge
|
1954
|
|
|
| Aircraft on photo: Folland Fo.139 Midge Photo source:Airwar.ru |
|
|
|
Manufacturer:
|
Folland Aircraft Limited, United Kingdom
|
Max speed:
|
966 km/h
|
(600 mph) |
Length: |
Type:
|
light fighter aircraft
|
Range: |
NA
|
|
Span:
|
Description:
|
small swept-wing British subsonic light fighter |
Ferry range:
|
1.852 km
|
(1.150 mi) |
Height:
|
| |
built as concept demonstrator for Folland Gnat
|
Ceiling: |
12.191 m
|
(40.000 ft)
|
Max weight: |
| First flight: |
1954 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
8,76 m
|
(28 ft 9 in)
|
6,30 m
|
(20 ft 8 in)
|
2,82 m
|
(9 ft 3 in)
|
2.041 kg
|
(4.500 lb)
|
| 1 |
|
| More info |
/sources: |
|
| Engine: |
1 × Armstrong Siddeley Viper 101 turbojet
|
|
|
| Thrust: |
1 x 7,295 kN (1 x 1.640 lbf)
|
|
|
| Armament: |
none
|
|
|
|
|
|
|
|
|
Gloster Trent-Meteor
|
1945 |
 |
|
Aircraft on photo: Gloster Trent-Meteor
|
|
| |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
NA
|
|
Length: |
Type:
|
experimental fighter
|
Range: |
NA
|
|
Span:
|
Description:
|
world's first turboprop-powered aircraft built |
Ferry range:
|
NA
|
|
Height:
|
| |
as a testbed for turboprop power development |
Ceiling: |
12.191 m
|
(40.000 ft)
|
Max weight: |
| First flight: |
1945 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
12,57 m
|
(41 ft 3 in)
|
13,12 m
|
(43 ft 1 in)
|
3,96 m
|
(13 ft 0 in)
|
6.260 kg
|
(13.800 lb)
|
| 1 |
|
| More info |
/sources: |
|
| Engine: |
2 x Rolls-Royce R.B.50 Trent turboprops
|
|
|
| Power/thrust: |
2 x 260 kW (2 x 350 KS) and 2 x 6,23 kN (2 x 1.400 lbf) residual thrust
|
|
|
| Armament: |
none
|
|
|
|
|
|
|
|
|
Gloster Meteor T.7
|
1948 |
 |
|
Aircraft on photo: Gloster Meteor T.7
|
|
| Data for: Gloster Meteor T.7 |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
941 km/h
|
(585 mph) |
Length: |
Type:
|
fighter-trainer
|
Range: |
NA
|
|
Span:
|
Description:
|
Meteor F.4 two-seat trainer variant |
Ferry range:
|
1.540 km
|
(957 mi) |
Height:
|
| First flight: |
1948 |
Ceiling: |
13.715 m
|
(45.000 ft)
|
Max weight: |
| Crew: |
2 |
Climb rate: |
38,6 m/s
|
(7.600 ft/min)
|
Number built: |
|
13,26 m
|
(43 ft 6 in)
|
11,32 m
|
(37 ft 2 in)
|
3,96 m
|
(13 ft 0 in)
|
7.983 kg
|
(18.000 lb)
|
| 654 (T.7) |
|
|
Engines:
|
2 x Rolls-Royce Derwent 8 turbojets
|
|
More info/sources: |
| Thrust: |
2 x 15,6 kN (2 x 3.500 lbf)
|
|
|
| Armament: |
none
|
|
|
|
|
|
|
|
|
Gloster Meteor F.8
|
1948 |
 |
|
| Aircraft on photo: Gloster Meteor F.8 |
|
| Data for: Gloster Meteor F.8 |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
965 km/h
|
(600 mph) |
Length: |
Type:
|
fighter
|
Range: |
965 km
|
(600 mi)
|
Span:
|
Description:
|
greatly improved F.4 with longer fuselage, |
Ferry range:
|
1.580 km
|
(982 mi)
|
Height:
|
| |
greater fuel capacity, standard ejection seat |
Ceiling: |
13.100 m
|
(43.000 ft)
|
Max weight: |
| |
and modified tail (derived from the E.1/44) |
Climb rate: |
35,6 m/s |
(7.000 ft/min)
|
Number built: |
| First flight: |
1948 |
Crew: |
1 |
|
|
|
13,59 m
|
(44 ft 7 in)
|
11,32 m
|
(37 ft 2 in)
|
3,96 m
|
(13 ft 0 in)
|
8.664 kg
|
(19.100 lb)
|
| 3.947 |
(total Meteor) |
| |
|
|
| Engines: |
2 x Rolls-Royce Derwent 8 turbojets
|
|
|
| Thrust: |
2 x 15,6 kN (2 x 3.500 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
| |
Rockets: 8-16 |
|
|
| |
Bombs: 2 x 454 kg (2 x 1.000 lb)
|
|
|
|
|
|
|
|
|
Gloster Reheat-Derwent Meteor
|
1949 |
 |
|
| Aircraft on photo: Gloster Reheat-Derwent Meteor Photo source: Thehangar.tv by Barry Jones |
|
| |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
NA
|
|
Length: |
Type:
|
experimental fighter
|
Range: |
NA
|
|
Span:
|
Description:
|
Meteor F.4 with Derwent reheat engines |
Ferry range:
|
NA
|
|
Height:
|
| First flight: |
1949 |
Ceiling: |
NA
|
|
Max weight: |
| Crew: |
1 |
Climb rate: |
NA |
|
Number built: |
|
12,5 m
|
(41 ft 0 in)
|
NA
|
|
3,96 m
|
(13 ft 0 in)
|
NA
|
|
| 3 |
|
|
| Engines: |
2 x Rolls-Royce Derwent 5 turbojets with reheat and variable area jet-nozzles
|
|
|
| Thrust: |
NA
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Gloster Meteor F.8 Soar turbojets
|
1953 |
 |
|
Aircraft on photo: Gloster Meteor F.8 Soar turbojets Photo source: Thehangar.tv by Barry Jones
|
|
|
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
NA
|
|
Length: |
Type:
|
experimental fighter
|
Range: |
NA
|
|
Span:
|
Description:
|
the first four engined jet aircraft with |
Ferry range:
|
NA
|
|
Height:
|
| |
Rolls-Royce Soar engines at wingtips |
Ceiling: |
NA
|
|
Max weight: |
| First flight: |
1953 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
13,59 m
|
(44 ft 7 in)
|
12 m
|
(39 ft 4 in)
|
3,96 m
|
(13 ft 0 in)
|
NA
|
|
| 1 |
|
| More info |
/sources: |
|
| Engines: |
2 x Rolls-Royce Derwent 8 turbojets
|
|
|
| |
2 x Rolls-Royce Soar disposable turbojets (with 10 h lifetime)
|
|
|
| Thrust: |
2 x 15,6 kN (2 x 3.500 lbf) Derwent
|
|
|
| |
2 x 8,05 kN (2 x 1.810 lbf) Soar |
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Gloster Meteor F.8 Prone Pilot
|
1954 |
 |
|
| Aircraft on photo: Gloster Meteor F.8 Prone Pilot Photo source: RCgroups.com |
|
| |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
965 km/h
|
(600 mph)
|
Length: |
Type:
|
experimental fighter
|
Range: |
965 km
|
(600 mi)
|
Span:
|
Description:
|
much modified Meteor F8 used to evaluate
|
Ferry range:
|
NA
|
|
Height:
|
| |
effects of G-forces while flying in a prone |
Ceiling: |
13.100 m
|
(43.000 ft)
|
Loaded weight: |
| |
position |
Climb rate: |
35,6 m/s
|
(7.000 ft/min)
|
Number built: |
| First flight: |
1954 |
Crew: |
2 |
|
|
|
15,9 m
|
(52 ft 5 in)
|
11,32 m
|
(37 ft 2 in)
|
3,96 m
|
(13 ft 0 in)
|
7.121 kg
|
(15.700 lb)
|
| 1 |
|
| |
|
|
| Engines: |
2 x Rolls-Royce Derwent 8 turbojets
|
|
|
| Thrust: |
2 x 15,6 kN (2 x 3.500 lbf)
|
|
|
| Armament: |
none
|
|
|
|
|
|
|
|
|
Gloster Jet Deflection Meteor
|
1954 |
 |
|
| Aircraft on photo: Gloster Jet Deflection Meteor Photo source: Thehangar.tv by Barry Jones |
|
(also called Westland / N.G.T.E. Meteor)
|
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
NA |
|
Length: |
Type:
|
experimental fighter
|
Min speed: |
130 km/h
|
(81 mph)
|
Span:
|
Description:
|
Meteor with Nene engines with thrust deflectors |
Range:
|
NA
|
|
Height:
|
| |
on the bottom of the engine nacelles, intended |
Ceiling: |
NA
|
|
Max weight: |
| |
to lower takeoff and landing speed |
Climb rate: |
NA |
|
Number built: |
| First flight: |
1954 |
Crew: |
1 |
|
|
|
13,59 m
|
(44 ft 7 in)
|
NA
|
|
3,96 m
|
(13 ft 0 in)
|
NA
|
|
| 1 |
|
| |
|
|
| Engines: |
2 × modified Rolls-Royce Nene 101 turbojets with deflection system
|
|
|
| Thrust: |
total thrust almost equal to the weight of the plane
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Gloster Meteor F.8 Screamer testbed
|
1955 |
 |
|
| Aircraft on photo: Gloster Meteor F.8 Screamer testbed Photo source: Thehangar.tv by Barry Jones |
|
| |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
NA
|
|
Length: |
Type:
|
experimental fighter
|
Range: |
NA
|
|
Span:
|
Description:
|
Meteor mixed propulsion version combining turbojets |
Ferry range:
|
NA
|
|
Height:
|
| |
and liquid-oxygene rocket engine to intercept |
Ceiling: |
NA
|
|
Max weight: |
| |
high-altitude bombers, project was canceled in 1956 |
Climb rate: |
NA |
|
Number built: |
| Completed: |
1955 |
Crew: |
1 |
|
|
|
13,59 m
|
(44 ft 7 in)
|
11,32 m
|
(37 ft 2 in)
|
3,96 m
|
(13 ft 0 in)
|
NA
|
|
| 1 |
|
| More info |
/sources: |
|
| Engines: |
2 x Rolls-Royce Derwent 8 turbojets
|
|
|
| |
1 x Armstrong-Siddeley Screamer rocket engine
|
|
|
| Thrust: |
2 x 15,6 kN (2 x 3.500 lbf) turbojets
|
|
|
| |
1 x 35,59 kN (1 x 8.000 lbf) rocket engine |
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Gloster Meteor U.15
|
1955 |
 |
|
| Aircraft on photo: Gloster Meteor U.15 |
|
| Data for: Gloster Meteor U.15 |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
941 km/h
|
(585 mph) |
Length: |
Type:
|
unmanned target drone
|
Range: |
NA
|
|
Span:
|
Description:
|
unmanned target drone created from Meteor F.4 |
Ferry range:
|
NA
|
|
Height:
|
| |
used to develop ground & air launched guided |
Ceiling: |
12.200 m
|
(40.025 ft)
|
Max weight: |
| |
missiles, which needed expendable targets |
Climb rate: |
NA |
|
Number built: |
| First flight: |
1955 |
Crew: |
0 / 1 |
|
|
|
12,50 m
|
(41 ft 0 in)
|
NA
|
|
3,96 m
|
(13 ft 0 in)
|
7.840 kg
|
(17.285 lb)
|
92 (U.15)
|
|
| |
|
|
| Engines: |
2 x Rolls-Royce Derwent 8 turbojets
|
|
|
| Thrust: |
2 x 15,6 kN (2 x 3.500 lbf)
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Gloster Meteor U.16 / U.21
|
1956 |
 |
|
| Aircraft on photo: Gloster Meteor U.16 |
|
| Data for: Gloster Meteor U.16 |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
962 km/h
|
(600 mph)
|
Length: |
Type:
|
unmanned target drone
|
Range: |
NA
|
|
Span:
|
Description:
|
unmanned target drone created from Meteor F.8 |
Ferry range:
|
1.540 km
|
(957 mi) |
Height:
|
| |
with modified extended nose and slenderer |
Ceiling: |
13.100 m
|
(43.000 ft)
|
Max weight: |
| |
camera pods |
Climb rate: |
NA
|
|
Number built: |
| First flight: |
1956 |
Crew: |
0 |
More
|
info/sources: |
|
13,60 m
|
(44 ft 7 in)
|
11,33 m
|
(37 ft 2 in)
|
3,96 m
|
(13 ft 0 in)
|
8.664 kg
|
(19.100 lb)
|
| 250 (U.16); |
23 (U.21) |
| Airwar |
|
|
| Engines: |
2 x Rolls-Royce Derwent RD.8 turbojets
|
|
|
| Thrust: |
2 x 17,48 kN (2 x 3.930 lbf)
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Armstrong Whitworth Meteor NF.11 / NF.13
|
1950 |
 |
|
Aircraft on photo: Armstrong Whitworth Meteor NF.11
|
|
| Data for: Armstrong Whitworth Meteor NF.11 |
|
Manufacturer:
|
Armstrong Whitworth Aircraft, United Kingdom
|
Max speed:
|
871 km/h
|
(541 mph)
|
Length: |
Type:
|
night fighter
|
Combat range: |
670 km
|
(415 mi)
|
Span:
|
Description:
|
based on Meteor T.7 but with F.3 longer wings |
Ferry range:
|
1.530 km
|
(950 mi) |
Height:
|
| |
and F.8 fuselage and tail, it had extended nose |
Ceiling: |
13.100 m
|
(43.000 ft)
|
Max weight: |
| |
with new radar & cannons moved into wings,
|
Climb rate: |
NA
|
|
Number built: |
| |
outboard of engines |
First flight: |
1950 |
|
Crew:
|
|
14,78 m
|
(48 ft 6 in)
|
13,11 m
|
(43 ft 1 in)
|
4,24 m
|
(13 ft 11 in)
|
9.980 kg
|
(22.000 lb)
|
| 334 (NF.11); |
40 (NF.13) |
| 2 |
|
|
| Engines: |
2 x Rolls-Royce Derwent RD.8 turbojets
|
|
|
| Thrust: |
2 x 16,5 kN (2 x 3.704 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
|
|
|
|
|
|
Armstrong Whitworth Meteor NF.12
|
1953 |
 |
|
Aircraft on photo: Armstrong Whitworth Meteor NF.12 Photo source: Flickr, by Aeroreg
|
|
| Data for: Armstrong Whitworth Meteor NF.12 |
|
Manufacturer:
|
Armstrong Whitworth Aircraft, United Kingdom
|
Max speed:
|
871 km/h
|
(541 mph)
|
Length: |
Type:
|
night fighter
|
Range: |
670 km
|
(415 mi)
|
Span:
|
Description:
|
longer nose version of the NF.11 with American |
Ferry range:
|
1.530 km
|
(950 mi)
|
Height:
|
| |
radar and slightly larger fin |
Ceiling: |
13.100 m
|
(43.000 ft)
|
Take off weight: |
| First flight: |
1953 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
2 |
|
|
|
|
|
15,20 m
|
(49 ft 10 in)
|
13,11 m
|
(43 ft 1 in)
|
4,24 m
|
(13 ft 11 in)
|
8.976 kg
|
(19.790 lb)
|
| 100 (NF.12) |
|
| |
|
|
| Engines: |
2 x Rolls-Royce Derwent RD.9 turbojets
|
|
|
| Thrust: |
2 x 16,7 kN (2 x 3.858 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
|
|
|
|
|
|
Armstrong Whitworth Meteor NF.14
|
1953 |
 |
|
| Aircraft on photo: Armstrong Whitworth Meteor NF.14 |
|
| Data for: Armstrong Whitworth Meteor NF.14 |
|
Manufacturer:
|
Armstrong Whitworth Aircraft, United Kingdom
|
Max speed:
|
930 km/h
|
(578 mph)
|
Length: |
Type:
|
night fighter
|
Range: |
720 km
|
(447 mi)
|
Span:
|
Description:
|
NF.11 with longer nose and new two-piece |
Ferry range:
|
1.530 km
|
(950 mi)
|
Height:
|
| |
blown canopy instead of heavy-framed one |
Ceiling: |
12.200 m
|
(40.025 ft)
|
Max weight: |
| First flight: |
1953 |
Climb rate: |
29,5 m/s |
(5.800 ft/min)
|
Number built: |
| Crew: |
2 |
|
|
|
|
|
15,50 m
|
(50 ft 10 in)
|
13,11 m
|
(43 ft 1 in)
|
4,24 m
|
(13 ft 11 in)
|
9.625 kg
|
(21.220 lb)
|
| 101 (NF.14) |
|
| |
|
|
| Engines: |
2 x Rolls-Royce Derwent RD.8 turbojets
|
|
|
| Thrust: |
2 x 16,5 kN (2 x 3.704 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
|
|
|
|
|
|
Armstrong Whitworth Meteor NF.11 SFECMAS ramjets
|
1954 |
 |
|
Aircraft on photo: Armstrong Whitworth Meteor NF.11 SFECMAS ramjets Photo source: Flight, May 1955
|
|
| |
|
Manufacturer:
|
Armstrong Whitworth Aircraft, United Kingdom
|
Max speed:
|
NA
|
|
Length: |
Type:
|
experimental fighter
|
Range: |
670 km
|
(415 mi)
|
Span:
|
Description:
|
converted by French SFECMAS by adding
|
Ferry range:
|
NA
|
|
Height:
|
| |
two ramjet units to the Derwent 8s |
Ceiling: |
13.100 m
|
(43.000 ft)
|
Max weight: |
| First flight: |
1954 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
14,78 m
|
(48 ft 6 in)
|
13,11 m
|
(43 ft 1 in)
|
4,24 m
|
(13 ft 11 in)
|
9.980 kg
|
(22.000 lb)
|
| 1 |
|
| |
|
|
| Engines: |
2 x Rolls-Royce Derwent RD.8 turbojets
|
|
|
| |
2 x SFECMAS S.600 (S.N.C.A.N. ARS.600) ramjets |
|
|
| Thrust: |
2 x 16,5 kN (2 x 3.704 lbf) turbojets
|
|
|
| |
2 x 4,89 kN (2 x 1.100 lbf) ramjets
|
|
|
| Armament: |
NA
|
|
|
|
|
|
|
|
|
Gloster G.42 (E.1/44) Ace
|
1948
|
|
|
Aircraft on photo: Gloster G.42 (E.1/44) Ace
|
|
| |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
998 km/h
|
(620 mph)
|
Length: |
Type:
|
fighter aircraft
|
Range: |
660 km
|
(410 mi)
|
Span:
|
Description:
|
all-metal single-seat fighter designed during |
Ferry range:
|
NA
|
|
Height:
|
| |
WW II bur finalized after the war |
Ceiling: |
13.400 m
|
(44.000 ft)
|
Loaded weight: |
| First flight: |
1948 |
Climb rate: |
16,5 m/s |
(3.200 ft/min)
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
11,59 m
|
(38 ft 0 in)
|
10,98 m
|
(36 ft 0 in)
|
3,56 m
|
(11 ft 8 in)
|
5.214 kg
|
(11.470 lb)
|
| 3 |
(total) |
| |
|
|
| Engine: |
1 x Rolls-Royce Nene II centrifugal flow turbojet
|
|
|
| Thrust: |
1 x 22,3 kN (1 x 5.000 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
| |
Bombs: 2 x 454 kg (2 x 1.000 lb) or
|
|
|
| |
Rockets: 8 |
|
|
|
|
|
|
|
|
Gloster G.42 (E.1/44) TX148
|
1949 |
 |
|
Aircraft on photo: Gloster G.42 (E.1/44) TX148 Photo source: Avia Deja Vu
|
|
| |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
998 km/h
|
(620 mph)
|
Length: |
Type:
|
fighter aircraft
|
Range: |
660 km
|
(410 mi)
|
Span:
|
Description:
|
E.1/44 with modified tail to improve handling |
Ferry range:
|
NA
|
|
Height:
|
| |
which was then used also for Meteor F.8 |
Ceiling: |
13.400 m
|
(44.000 ft)
|
Loaded weight: |
| First flight: |
1949 |
Climb rate: |
16,5 m/s |
(3.200 ft/min)
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
11,59 m
|
(38 ft 0 in)
|
10,98 m
|
(36 ft 0 in)
|
3,56 m
|
(11 ft 8 in)
|
5.214 kg
|
(11.470 lb)
|
| 1 (TX148) |
|
| |
|
|
| Engine: |
1 x Rolls-Royce Nene II centrifugal flow turbojet
|
|
|
| Thrust: |
1 x 22,3 kN (1 x 5.000 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
| |
Bombs: 2 x 454 kg (2 x 1.000 lb) or
|
|
|
| |
Rockets: 8 |
|
|
|
|
|
|
|
|
Gloster CXP-1001 (mock up)
|
1949
|
|
|
Aircraft on photo: Gloster CXP-1001
|
|
| |
|
Manufacturer:
|
Gloster Aircraft Company, United Kingdom
|
Max speed:
|
965 km/h
|
(600 mph)
|
Length: |
Type:
|
experimental fighter
|
Range: |
660 km
|
(410 mi)
|
Span:
|
Description:
|
single-seater designed around the existing |
Ferry range:
|
1.600 km
|
|
Height:
|
| |
Rolls-Royce Nene turbojet developed for Taiwan |
Ceiling: |
12.200 m
|
(40.025 ft)
|
Max weight: |
| Canceled: |
1949 |
Climb rate: |
NA |
|
Number built: |
| Crew: |
1 |
|
|
|
|
|
12,75 m
|
(41 ft 10 in)
|
11,58 m
|
(38 ft 0 in)
|
4,51 m
|
(14 ft 2 in)
|
8.415 kg
|
(18.550 lb)
|
| 1 mock up |
|
| More info/ |
sources: |
|
| Engine: |
1 x Rolls-Royce Nene turbojet
|
|
|
| Thrust: |
1 x 22,5 kN (1 x 5.000 lbf)
|
|
|
| Armament: |
Guns: 4 x 20 mm (4 x 0.79 in)
|
|
|
|
|
|
|
|
|
Gloster GA.5
|
1951 |
 |
|
| Aircraft on photo: Gloster GA.5 WD804 (first prototype) Photo source: bt.internet.com |
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| Data for: Gloster GA.5 WD804 (first prototype) |
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Manufacturer:
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Gloster Aircraft Company, United Kingdom
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Max speed:
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Mach 1
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Length: |
Type:
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fighter prototype
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Range: |
NA
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Span:
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Description:
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Javelin prototype with shorter nose, pure delta |
Ferry range:
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NA |
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Height:
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wing (first 3 aircraft) and closed navigator rear
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Ceiling: |
NA |
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Max weight: |
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canopy (first 4 aircraft) |
Climb rate: |
NA |
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Number built: |
| First flight: |
1951 |
Crew: |
2 |
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16,7 m
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(54 ft 10 in)
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15,5 m
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(50 ft 10 in)
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4,88 m
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(16 ft 0 in)
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NA
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| 5 |
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| More info |
/sources: |
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| Engines: |
2 × Armstrong Siddeley Sapphire turbojets
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| Thrust: |
2 x 33,36 kN (2 x 7.500 lbf)
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Source: |
| Armament: |
none
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Flying Magazine, July 1952 |
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Gloster GA.5 "round radome"
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1953 |
 |
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| Aircraft on photo: Gloster GA.5 WT827 "round radome" Photo source: hydroponicsonline.com |
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Manufacturer:
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Gloster Aircraft Company, United Kingdom
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Max speed:
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Mach 0,95
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(est)
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Length: |
Type:
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fighter prototype
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Range: |
NA
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Span:
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Description:
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third Javelin prototype with round radome (that
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Ferry range:
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NA |
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Height:
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was later changed to the sharp point radome) |
Ceiling: |
NA |
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Max weight: |
| First flight: |
1953 |
Climb rate: |
NA |
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Number built: |
| Crew: |
2 |
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|
NA
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15,5 m
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(50 ft 10 in)
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4,88 m
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(16 ft 0 in)
|
NA
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| 1 |
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| More info |
/sources: |
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| Engines: |
2 × Armstrong Siddeley Sapphire Sa.6 turbojets
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| Thrust: |
2 x 36,92 kN (2 x 8.300 lbf)
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| Armament: |
Guns: 4 x 30 mm (4 x 1.18 in)
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Gloster Javelin
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1956
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Aircraft on photo: Gloster Javelin FAW.9 Photo source: Internet
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| Data for: Gloster Javelin FAW.9 |
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Manufacturer:
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Gloster Aircraft Company, United Kingdom
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Max speed:
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1.140 km/h
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(710 mph)
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Length: |
Type:
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all-weather fighter / interceptor
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Range: |
1.530 km |
(950 mi) |
Span:
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Description:
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T-tailed cranked delta-wing aircraft designed
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Ferry range:
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NA
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Height:
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for night and all-weather operations and the |
Ceiling: |
15.865 m
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(52.800 ft)
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Max weight: |
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last aircraft under Gloster name |
Climb rate: |
27,45 m
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(5.400 f/min) |
Number built: |
| First flight: |
1951 (GA.5); 1956 (FAW.1)
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Crew: |
2 |
More
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info/sources: |
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17,15 m
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(56 ft 9 in)
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15,85 m
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(52 ft 0 in)
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4,88 m
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(16 ft 0 in)
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19.580 kg
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(43.165 lb)
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| 436 |
(total) |
| Wikipedia |
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| Engines: |
2 × Armstrong Siddeley Sapphire 7R turbojets
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| Thrust: |
2 x 54 kN (2 x 12.300 lbf) with reheat
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| Armament: |
Guns: 4 x 30 mm (4 x 1.18 in)
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Missiles: 4 x air-to-air
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Gloster Javelin T
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1956 |
 |
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| Aircraft on photo: Gloster Javelin T.3 |
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| Data for: Gloster Javelin T.3 |
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Manufacturer:
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Gloster Aircraft Company, United Kingdom
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Max speed:
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1.115 km/h
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(695 mph)
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Length: |
Type:
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fighter-trainer
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Range: |
NA |
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Span:
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Description:
|
Javelin training version |
Ferry range:
|
NA
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Height:
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| First flight: |
1956 |
Ceiling: |
14.020 m
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(46.000 ft)
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Max weight: |
| Crew: |
2 |
Climb rate: |
NA
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Number built: |
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18,26 m
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(59 ft 11 in)
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15,85 m
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(52 ft 0 in)
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4,88 m
|
(16 ft 0 in)
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19.050 kg
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(42.000 lb)
|
| 23 |
(trainers) |
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| Engines: |
2 × Armstrong Siddeley Sapphire 6 turbojets
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More info/sources: |
| Thrust: |
2 x 35,6 kN (2 x 8.000 lbf)
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| Armament: |
Guns: 4 x 30 mm (4 x 1.18 in)
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