I
1903 – 1909
Control, not power
No contest
Everyone had an engine light enough by 1903. Only the Wrights had roll control, and they kept it to themselves for five years while they tried to sell it. There is no pendulum here because there is nothing to contest: the aeroplane cannot yet carry a gun, a useful load, or itself very far.
- Crew
- 2
- Engine
- Wright Vertical 4 — 4-cylinder water-cooled in-line piston engine
- Power
- 35 hp
- Max speed
- 68 km/h
- Ceiling
- 120 m
- Climb
- Not recorded
- Endurance
- about 1 hour
- Wingspan
- 11.10 m
- Length
- 9.35 m
- Wing area
- 46.0 m²
- Empty wt
- 336 kg
- Loaded wt
- 573 kg
- Wing loading
- 12.5 kg/m²
- Armament
- None — these types carried no fixed armament
- Built
- ≈15 (all Wright Model A)
- Crew
- 1
- Engine
- Anzani 3-cyl. fan — 3-cyl. air-cooled fan-style radial piston engine
- Power
- 25 hp
- Max speed
- 76 km/h
- Ceiling
- 1,000 m
- Climb
- Not recorded
- Endurance
- about 3 hours 30
- Wingspan
- 7.79 m
- Length
- 7.62 m
- Wing area
- 14.0 m²
- Empty wt
- 230 kg
- Loaded wt
- 300 kg
- Wing loading
- 21.4 kg/m²
- Armament
- None — these types carried no fixed armament
- Built
- ≈900
II
1909 – Aug 1914
A machine you can buy
No contest
The Gnome rotary made the aeroplane a product: light, air-cooled and reliable enough to sell to a customer. Armies bought them to look over the hill. Germany's edge in 1914 was not aerodynamic at all — it was the Zeppelin, which is what drove French and British aviation budgets. The aeroplane's job was still reconnaissance, and the B.E.2 was designed to be so stable it would fly itself while the observer worked.
- Crew
- 2
- Engine
- Mercedes D.I — 6-cyl. water-cooled piston engine
- Power
- 100 hp
- Max speed
- 100 km/h
- Ceiling
- 2,000 m
- Climb
- 792 m (2,600 ft) in 6 mins
- Endurance
- 4 hours
- Wingspan
- 14.35 m
- Length
- 9.80 m
- Wing area
- 27.9 m²
- Empty wt
- 650 kg
- Loaded wt
- 850 kg
- Wing loading
- 30.5 kg/m²
- Armament
- None — these types carried no fixed armament
- Built
- ≈500 (all builders)
- Crew
- 1
- Engine
- Gnome Lambda Lambda — air cooled 14-cylinder two-row rotary
- Power
- 160 hp
- Max speed
- 201 km/h
- Ceiling
- 3,000 m
- Climb
- Not recorded
- Endurance
- Not recorded
- Wingspan
- 6.65 m
- Length
- 6.10 m
- Wing area
- 9.7 m²
- Empty wt
- 350 kg
- Loaded wt
- 612 kg
- Wing loading
- 63.1 kg/m²
- Armament
- None — these types carried no fixed armament
- Built
- ≈40 (Monocoque racers)
- Crew
- Two
- Engine
- RAF 1a — V-8 air-cooled piston engine
- Power
- 90 hp
- Max speed
- 116 km/h
- Ceiling
- 3,048 m
- Climb
- / :*3500 ft in 6 minutes 30 seconds :*10000 ft in 45 minutes 15 seconds
- Endurance
- 3 hours 15 minutes
- Wingspan
- 11.28 m
- Length
- 8.31 m
- Wing area
- 34.5 m²
- Empty wt
- 621 kg
- Loaded wt
- 1,068 kg
- Wing loading
- 31.0 kg/m²
- Armament
- Normally; 1 × .303 in Lewis gun for observer, sometimes several
- Built
- ~ 3,500
—
1914 – 1918 has its own page
The First World War is where the pendulum swings fastest and where it is easiest to see, because one front and two sides is the whole picture. Eight eras, eighteen aircraft, the Fokker Scourge through to the D.VII.
The Fighter Pendulum — WWI →
III
1919 – 1926
The plateau
Nobody
The enabling change of this era is the absence of one. Disarmament, warehouses of surplus wartime airframes and no budget anywhere. Engines improved steadily; airframes stayed wood, wire and fabric for a decade, because the tactical lesson everyone drew from 1918 was that fights are won by out-turning the other man at low speed — and a biplane does that.
- Crew
- 1
- Engine
- Hispano-Suiza 8Fb V-8 piston engine
- Power
- 300 hp
- Max speed
- 235 km/h
- Ceiling
- 8,500 m
- Climb
- 6.1 m/s
- Range
- 580 km
- Wingspan
- 9.70 m
- Length
- 6.49 m
- Wing area
- 26.7 m²
- Empty wt
- 760 kg
- Loaded wt
- 1,150 kg
- Wing loading
- 43.1 kg/m²
- Armament
- 2 × fixed forward-firing 7.7 mm Vickers machine guns
- Built
- 1571 ca
- Crew
- 1
- Engine
- Armstrong Siddeley Jaguar IV — 14-cylinder air-cooled radial piston engine
- Power
- 400 hp
- Max speed
- 245 km/h
- Ceiling
- 7,010 m
- Climb
- 20000 ft in 23 minutes
- Endurance
- 2 hours 45 minutes
- Wingspan
- 8.94 m
- Length
- 6.17 m
- Wing area
- 23.6 m²
- Empty wt
- 780 kg
- Loaded wt
- 1,189 kg
- Wing loading
- 50.4 kg/m²
- Armament
- 2 × 0.303 in Vickers machine guns
- Built
- 133
- Crew
- one
- Engine
- Curtiss D-12 — water-cooled V-12
- Power
- 435 hp
- Max speed
- 256 km/h
- Ceiling
- 5,768 m
- Climb
- 8.3 m/s
- Range
- 628 km
- Wingspan
- 9.75 m
- Length
- 7.14 m
- Wing area
- 24.2 m²
- Empty wt
- 878 kg
- Loaded wt
- 1,415 kg
- Wing loading
- 58.5 kg/m²
- Armament
- 2 × fixed .30 in machine guns
- Built
- 158
IV
1927 – 1933
The racers do the research
Technical lead — Britain, Italy, USA
No air ministry would pay for the aerodynamic work the next fighter needed. Air racing did. The Schneider Trophy took Rolls-Royce from the R engine to the Merlin; the American circuit and NACA produced the drag cowling; stressed-skin metal and retractable gear arrived as answers to racing problems. The Hawker Fury is the biplane at its absolute peak, and a dead end. The S.6B is not a fighter and is here because it is where the Spitfire's engine came from.
- Crew
- 1
- Engine
- Rolls-Royce R — V-12 liquid-cooled piston engine
- Power
- 2,350 hp
- Max speed
- 656 km/h
- Ceiling
- 4,000 m
- Climb
- Not recorded
- Endurance
- Not recorded — a closed-circuit racer
- Wingspan
- 9.14 m
- Length
- 8.79 m
- Wing area
- 13.5 m²
- Empty wt
- 2,082 kg
- Loaded wt
- 2,761 kg
- Wing loading
- 204.5 kg/m²
- Armament
- None — a Schneider Trophy racer, not a fighter
- Built
- 2
- Crew
- 1
- Engine
- Rolls-Royce Kestrel IV — liquid-cooled V12 engine
- Power
- 640 hp
- Max speed
- 359 km/h
- Ceiling
- 8,992 m
- Climb
- 3 min 50 s to 10000 ft
- Range
- 435 km
- Wingspan
- 9.14 m
- Length
- 8.15 m
- Wing area
- 23.4 m²
- Empty wt
- 1,240 kg
- Loaded wt
- 1,637 kg
- Wing loading
- 70.0 kg/m²
- Armament
- 2 × 0.303 in (7.7 mm) Vickers Mk IV machine guns with 600 rpg
- Built
- 275
- Crew
- 1
- Engine
- Pratt & Whitney R-1340-27 Wasp — 9-cylinder air-cooled radial piston engine
- Power
- 600 hp
- Max speed
- 377 km/h
- Ceiling
- 8,352 m
- Climb
- 3.7 m/s
- Range
- 579 km
- Wingspan
- 8.53 m
- Length
- 7.19 m
- Wing area
- 23.2 m²
- Empty wt
- 996 kg
- Loaded wt
- 1,524 kg
- Wing loading
- 65.7 kg/m²
- Armament
- 2 × .30 in M1919 Browning machine guns or 1 x .30 in and 1 x .50 in machine guns
- Built
- 151
V
1934 – 1936
The monoplane revolution
Edge — Soviet
The Polikarpov I-16 was the first cantilever monoplane fighter with retractable undercarriage in service anywhere, and over Madrid in 1936 it humiliated the Heinkel He 51. The enabling change was not the airframe but the concession that followed it: Germany accepted that the biplane era was over and stopped arguing. Note what the stat cards show — the I-16's wing loading is more than double the CR.32's. That is the whole argument between angle fighting and energy fighting, in one number.
- Crew
- 1
- Engine
- Shvetsov M-63 — 9-cylinder supercharged air-cooled radial engine
- Power
- 1,100 hp
- Max speed
- 489 km/h
- Ceiling
- 9,700 m
- Climb
- 14.7 m/s
- Range
- 700 km
- Wingspan
- 9.00 m
- Length
- 6.13 m
- Wing area
- 14.5 m²
- Empty wt
- 1,490 kg
- Loaded wt
- 1,941 kg
- Wing loading
- 133.9 kg/m²
- Armament
- 2 × fixed forward-firing 7.62 mm ShKAS machine guns in upper cowling; 2 × fixed forward-firing 7.62 mm ShKAS machine guns in the wings/ 20 mm ShVAK cannons (type-28); 6 × unguided RS-82 rockets or up to 500 kg of bombs
- Built
- 10,292 (6,848 fighters and 3,444 trainers)
- Crew
- 1
- Engine
- Shvetsov M-25 — 9-cylinder air-cooled radial piston engine
- Power
- 700 hp
- Max speed
- 367 km/h
- Ceiling
- 9,800 m
- Climb
- / 1.1 min to 1000 m 6.1 min to 5000 m
- Range
- 510 km
- Wingspan
- 9.75 m
- Length
- 6.10 m
- Wing area
- 21.9 m²
- Empty wt
- 1,012 kg
- Loaded wt
- 1,385 kg
- Wing loading
- 63.2 kg/m²
- Armament
- 4 x7.62×54mmR PV-1 machine guns Up to 100 kg (220 lb) of bombs
- Built
- 3,313 (plus 3,437 I-153)
- Crew
- 1
- Engine
- Fiat A.30 R.A.bis — V-12 liquid-cooled piston engine
- Power
- 599 hp
- Max speed
- 360 km/h
- Ceiling
- 8,800 m
- Climb
- 9.0 m/s
- Range
- 781 km
- Wingspan
- 9.50 m
- Length
- 7.47 m
- Wing area
- 22.1 m²
- Empty wt
- 1,455 kg
- Loaded wt
- 1,975 kg
- Wing loading
- 89.4 kg/m²
- Armament
- 2 × 7.7 mm or 12.7 mm Breda-SAFAT machine guns
- Built
- 1,052
- Crew
- 1
- Engine
- BMW VI 7.3 Z — V-12 liquid-cooled piston engine
- Power
- 750 hp
- Max speed
- 330 km/h
- Ceiling
- 7,700 m
- Climb
- 1000 m in 1 minute 24 seconds 6000 m in 16 minute 30 seconds
- Range
- 570 km
- Wingspan
- 11.00 m
- Length
- 8.40 m
- Wing area
- 27.2 m²
- Empty wt
- 1,460 kg
- Loaded wt
- 1,900 kg
- Wing loading
- 69.9 kg/m²
- Armament
- 2 × 7.92 mm MG 17 machine guns in nose; 500 rpg
- Built
- 700
- Crew
- 1
- Engine
- PZL Bristol Mercury VI S2 — 9-cyl. air-cooled radial piston engine
- Power
- 645 hp
- Max speed
- 390 km/h
- Ceiling
- 8,000 m
- Climb
- / 5,000 m in 6 minutes 7,000 m in 13 minutes
- Range
- 700 km
- Wingspan
- 10.72 m
- Length
- 7.55 m
- Wing area
- 17.9 m²
- Empty wt
- 1,147 kg
- Loaded wt
- 1,630 kg
- Wing loading
- 91.1 kg/m²
- Armament
- 2 x 7.92 mm wz. 33 machine guns in fuselage with 500 rpg. optionally additional; 2 × 7.92 mm wz. 33 machine guns in wings with 300 rpg
- Built
- 325
VI
1936 – 1938
Spain settles it
Edge — Germany
Two things, neither of them the airframe. Direct fuel injection in the DB 601 kept running under negative g where a float-carburettor Merlin cut out; and the Rotte and Schwarm, worked out by Mölders over Spain, put two and four aircraft into a flexible fighting formation while the RAF and the Armée de l'Air still flew rigid three-aircraft vics. Britain's answer was ordered but not yet delivered.
- Crew
- 1
- Engine
- Daimler-Benz DB 605A — V-12 inverted liquid-cooled piston engine
- Power
- 1,455 hp
- Max speed
- 640 km/h
- Ceiling
- 11,550 m
- Climb
- 17.0 m/s
- Range
- 850 km
- Wingspan
- 9.92 m
- Length
- 8.95 m
- Wing area
- 16.1 m²
- Empty wt
- 2,247 kg
- Loaded wt
- 3,148 kg
- Wing loading
- 196.1 kg/m²
- Armament
- 1 × 20 mm MG 151/20 through the propeller hub; 2 × 13 mm MG 131
- Built
- 34,248 (all marks)
- Crew
- 1
- Engine
- Nakajima Kotobuki 41 or 41 KAI — 9-cylinder air-cooled radial piston engine
- Power
- 710 hp
- Max speed
- 435 km/h
- Ceiling
- 9,800 m
- Climb
- 3000 m in 3 minutes 35 seconds
- Range
- 1,200 km
- Wingspan
- 11.00 m
- Length
- 7.57 m
- Wing area
- 17.8 m²
- Empty wt
- 1,216 kg
- Loaded wt
- 1,671 kg
- Wing loading
- 93.9 kg/m²
- Armament
- 2 × 7.7 mm Type 97 aircraft machine gun fuselage-mounted synchronized machine guns firing through the engine cylinders and propeller at about 1 and 11 o'clock
- Built
- 1,094
- Crew
- 1
- Engine
- Bristol Mercury IX — nine-cylinder air-cooled radial piston engine
- Power
- 830 hp
- Max speed
- 407 km/h
- Ceiling
- 9,997 m
- Climb
- 11.7 m/s
- Endurance
- 2 hours
- Wingspan
- 9.83 m
- Length
- 8.36 m
- Wing area
- 30.0 m²
- Empty wt
- 1,459 kg
- Loaded wt
- 2,084 kg
- Wing loading
- 69.5 kg/m²
- Armament
- Initially: two synchronised .303 in Vickers machine guns in fuselage sides, two .303 in Lewis machine guns; one beneath each lower wing. Later aircraft: four Browning .303 Mark II machine guns, two synchronised gun
- Built
- 747
VII
Sep 1939 – Jun 1940
The Luftwaffe is a system, not a Bf 109
Edge — Germany
The Bf 109 E was not decisively better than a Hurricane. What surrounded it was: a radio in every cockpit, the Schwarm, ground-to-air liaison, and commanders who concentrated fighters where they mattered. The Bf 110 was supposed to be the long-range weapon and was found out within a year.
- Crew
- two or three
- Engine
- Daimler-Benz DB 601A-1 — V-12 inverted liquid-cooled piston engines
- Power
- 2 × 1,050 hp
- Max speed
- 475 km/h
- Ceiling
- 10,000 m
- Climb
- 11.0 m/s
- Range
- 774 km
- Wingspan
- 16.25 m
- Length
- 12.07 m
- Wing area
- 38.4 m²
- Empty wt
- 4,425 kg
- Loaded wt
- 6,028 kg
- Wing loading
- 157.0 kg/m²
- Armament
- 2 × 20 mm MG FF/M cannon (180 rpg—3 drums with 60 rpg, cannon were reloaded by rear gunner or radio operator during flight); 4 × 7.92 mm MG 17 machine guns (1,000 rpg); 1 × 7.92 mm MG 15 machine gun for defence
- Built
- 6,170
- Crew
- 1
- Engine
- Rolls-Royce Merlin XX — V-12 liquid-cooled piston engine
- Power
- 1,185 hp
- Max speed
- 547 km/h
- Ceiling
- 10,973 m
- Climb
- 14.1 m/s
- Range
- 966 km
- Wingspan
- 12.19 m
- Length
- 9.83 m
- Wing area
- 23.9 m²
- Empty wt
- 2,606 kg
- Loaded wt
- 3,479 kg
- Wing loading
- 145.6 kg/m²
- Armament
- 4 × 20 mm Hispano Mk II cannon
- Built
- 14,487 (UK and Canada)
Where the bar is lying
NW Europe
Eastern FrontNot yet a front
MediterraneanNot yet a front
PacificNot yet a front
VIII
Jul 1940 – May 1941
The Dowding System
Edge — Britain, defensively
The margin was on the ground. Chain Home, the filter room and sector control made the first working integrated air defence network, turning interception from luck into a process. The aeroplanes mattered — 100-octane fuel and constant-speed propellers improved the ones already in service — but a Spitfire without the system behind it is just a fast aeroplane in a large sky.
No challengerNothing on this side set a standard the other had to answer.
- Crew
- 1
- Engine
- Rolls-Royce Merlin 45 — V-12 liquid-cooled piston engine
- Power
- 1,470 hp
- Max speed
- 595 km/h
- Ceiling
- 11,125 m
- Climb
- 13.2 m/s
- Range
- 399 km
- Wingspan
- 11.23 m
- Length
- 9.12 m
- Wing area
- 22.5 m²
- Empty wt
- 2,297 kg
- Loaded wt
- 3,004 kg
- Wing loading
- 133.5 kg/m²
- Armament
- A wing; 8 × .303 in Browning Mk IImachine guns (350 rounds per gun) B wing; 2 × 20 mm Hispano Mk II (60 rounds per gun); 4 × .303 in Browning Mk IImachine guns (350 rounds per gun) C wing; 4 × 20 mm Hispano Mk II
- Built
- More than 20,351
Where the bar is lying
NW Europe
Eastern FrontNot yet a front
MediterraneanAxis-held; the bar does not describe Malta or the Western Desert
PacificNot yet a front
IX
Jun 1941 – Jun 1942
Two shocks, on two different clocks
Edge — Axis, in both hemispheres
The Fw 190 arrived over France and comprehensively beat the Spitfire V; its enabling piece was the Kommandogerät, a single-lever engine computer that let a tired pilot fly the BMW 801 properly. The A6M's advantage was not technology but range and a small cadre of superbly trained naval aircrew — an asset that could not be replaced once spent. This is the era where a single global bar is least honest, and the strip below is where it admits it.
- Crew
- 1
- Engine
- BMW 801D-2 — 14-cylinder air-cooled radial piston engine
- Power
- 1,677 hp
- Max speed
- 652 km/h
- Ceiling
- 10,350 m
- Climb
- 15.0 m/s
- Range
- 400 km
- Wingspan
- 10.51 m
- Length
- 8.95 m
- Wing area
- 18.3 m²
- Empty wt
- 3,200 kg
- Loaded wt
- 4,417 kg
- Wing loading
- 241.4 kg/m²
- Armament
- 2 × 13 mm synchronized MG 131 machine guns; 2 × 20 mm MG 151/20 E cannons, synchronized in the wing roots; 2 × 20 mm MG 151/20 E cannons in mid-wing mounts
- Built
- Over 20,000
- Crew
- 1
- Engine
- Nakajima NK1C Sakae-12 — 14-cylinder air-cooled radial piston engine
- Power
- 940 hp
- Max speed
- 533 km/h
- Ceiling
- 10,000 m
- Climb
- 15.7 m/s
- Range
- 1,870 km
- Wingspan
- 12.00 m
- Length
- 9.06 m
- Wing area
- 22.4 m²
- Empty wt
- 1,680 kg
- Loaded wt
- 2,796 kg
- Wing loading
- 124.6 kg/m²
- Armament
- thumb|Divergence of trajectories between 7.7 mm and 20 mm ammunition; 2 × 7.7 mm Type 97 aircraft machine guns in the engine cowling, with 500 rounds per gun. 2 × 20 mm Type 99-1 Mk.3 cannon in the wings, with 60 rounds
- Built
- 10,939
- Crew
- 1
- Engine
- Nakajima Ha-115 — 14-cylinder air-cooled radial piston engine
- Power
- 1,300 hp
- Max speed
- 530 km/h
- Ceiling
- 11,200 m
- Climb
- 5000 m in five minutes and 49 seconds
- Range
- 1,760 km
- Wingspan
- 10.84 m
- Length
- 8.92 m
- Wing area
- 21.4 m²
- Empty wt
- 1,910 kg
- Loaded wt
- 2,590 kg
- Wing loading
- 121.0 kg/m²
- Armament
- 2 × 12.7 mm Ho-103's in the forward fuselage with 270 rpg
- Built
- 5,919
- Crew
- 1
- Engine
- Pratt & Whitney R-1830-76 — 14-cylinder air-cooled radial piston engine
- Power
- 1,200 hp
- Max speed
- 533 km/h
- Ceiling
- 12,040 m
- Climb
- 11.7 m/s
- Range
- 1,360 km
- Wingspan
- 11.58 m
- Length
- 8.76 m
- Wing area
- 24.2 m²
- Empty wt
- 2,226 kg
- Loaded wt
- 3,367 kg
- Wing loading
- 139.1 kg/m²
- Armament
- 4 × 0.50 in (12.7 mm) AN/M2 Browning machine guns with 450 rounds per gun
- Built
- 7,885
- Crew
- 1
- Engine
- Mikulin AM-35A — V-12 liquid-cooled piston engine
- Power
- 1,332 hp
- Max speed
- 505 km/h
- Ceiling
- 12,000 m
- Climb
- 8000 m in 10 minutes 17 seconds
- Range
- 820 km
- Wingspan
- 10.20 m
- Length
- 8.25 m
- Wing area
- 17.4 m²
- Empty wt
- 2,699 kg
- Loaded wt
- 3,355 kg
- Wing loading
- 192.4 kg/m²
- Armament
- 1 × 12.7 mm Berezin UBS machine gun :2 × 7.62 mm ShKAS machine guns in the cowl :(later models would feature additional; 2 × UBK machine guns underwing, one per wing)
- Built
- 3,422
- Crew
- 1
- Engine
- Allison V-1710-39 — V-12 liquid-cooled piston engine
- Power
- 1,240 hp
- Max speed
- 581 km/h
- Ceiling
- 8,870 m
- Climb
- 15000 ft in 6 minutes 15 seconds
- Range
- 1,152 km
- Wingspan
- 11.37 m
- Length
- 9.66 m
- Wing area
- 21.9 m²
- Empty wt
- 2,686 kg
- Loaded wt
- 3,760 kg
- Wing loading
- 171.7 kg/m²
- Armament
- 6 × 0.5 in M2 Browning machine guns in the wings
- Built
- 13,738
Where the bar is lying
NW EuropeFw 190 A over the Channel
Eastern FrontCatastrophic Soviet losses, June–December 1941
Mediterranean
PacificZero unanswered until mid-1942
X
Jul 1942 – 1943
The answers arrive
Swings — Allied
The single most important object of the air war is not an aeroplane: it is the two-stage two-speed supercharger, married to 100/130-octane fuel. The Spitfire IX was a Mk V airframe with a Merlin 61 dropped into it, in service within months of the Fw 190 shock. In the Pacific there was no technical fix required at all — Japan lost its trained aircrew at Midway and Guadalcanal and had no pipeline to replace them.
- Crew
- 1
- Engine
- Alfa Romeo RA.1000 R.C.41-I Monsone — V-12 inverted liquid-cooled piston engine
- Power
- 1,159 hp
- Max speed
- 600 km/h
- Ceiling
- 11,500 m
- Climb
- 18.1 m/s
- Range
- 765 km
- Wingspan
- 10.58 m
- Length
- 8.85 m
- Wing area
- 16.8 m²
- Empty wt
- 2,491 kg
- Loaded wt
- 2,930 kg
- Wing loading
- 174.2 kg/m²
- Armament
- 2 × 12.7 mm Breda-SAFAT machine guns in the engine cowling, 360/400 rpg; 2 × 7.7 mm Breda-SAFAT machine guns in the wings, 500 rpg; 2 × 50 kg, 100 kg or 160 kg bombs
- Built
- 1,150
- Crew
- 1
- Engine
- Nakajima NK9H Homare 21 — 18-cylinder air-cooled radial piston engine
- Power
- 1,975 hp
- Max speed
- 571 km/h
- Ceiling
- 12,009 m
- Climb
- 19.7 m/s
- Range
- 1,078 km
- Wingspan
- 12.00 m
- Length
- 8.88 m
- Wing area
- 23.5 m²
- Empty wt
- 2,897 kg
- Loaded wt
- 3,900 kg
- Wing loading
- 166.0 kg/m²
- Armament
- 4 × 20 mm Type 99 Mark 2 machine guns in the wings
- Built
- 1,532
- Crew
- 1
- Engine
- Pratt & Whitney R-2800-10W Double Wasp — 18-cylinder air-cooled radial piston engine
- Power
- 2,200 hp
- Max speed
- 629 km/h
- Ceiling
- 11,369 m
- Climb
- 13.2 m/s
- Range
- 1,521 km
- Wingspan
- 13.06 m
- Length
- 10.24 m
- Wing area
- 31.0 m²
- Empty wt
- 4,190 kg
- Loaded wt
- 5,714 kg
- Wing loading
- 184.3 kg/m²
- Armament
- 6 × 0.50 in (12.7 mm) M2 Browning machine guns, with 400 rounds per gun, (All F6F-3, and most F6F-5) or; 2 × 0.79 in (20 mm) AN/M2 cannon, with 225 rounds per gun and; 4 × 0.50 in (12.7 mm) Browning machine guns with 400
- Built
- 12,275
- Crew
- 1
- Engine
- Allison V-1710 (-111 left hand rotation and -113 right hand rotation) — V-12 liquid-cooled turbo-supercharged piston engine
- Power
- 2 × 1,600 hp
- Max speed
- 666 km/h
- Ceiling
- 13,411 m
- Climb
- 24.1 m/s
- Range
- 2,092 km
- Wingspan
- 15.85 m
- Length
- 11.53 m
- Wing area
- 30.4 m²
- Empty wt
- 5,806 kg
- Loaded wt
- 7,938 kg
- Wing loading
- 261.1 kg/m²
- Armament
- 1× Hispano M2(C) 20 mm cannon with 150 rounds; 4× M2 Browning machine gun 0.50 in (12.7 mm) machine guns with 500 rpg
- Built
- 10,037
- Crew
- 1
- Engine
- Shvetsov M-82FN — 14-cylinder air-cooled radial piston engine
- Power
- 1,958 hp
- Max speed
- 648 km/h
- Ceiling
- 11,000 m
- Climb
- 16.7 m/s
- Range
- 765 km
- Wingspan
- 9.80 m
- Length
- 8.67 m
- Wing area
- 17.5 m²
- Empty wt
- 2,706 kg
- Loaded wt
- 3,168 kg
- Wing loading
- 181.0 kg/m²
- Armament
- 2 × 20 mm ShVAK cannon with 170 rpg
- Built
- 9,920
- Crew
- 1
- Engine
- Klimov VK-105PF2 — V-12 liquid-cooled piston engine
- Power
- 1,290 hp
- Max speed
- 646 km/h
- Ceiling
- 10,400 m
- Climb
- 5000 m in 4 minutes 30 seconds
- Range
- 550 km
- Wingspan
- 9.20 m
- Length
- 8.50 m
- Wing area
- 14.8 m²
- Empty wt
- 2,105 kg
- Loaded wt
- 2,697 kg
- Wing loading
- 181.6 kg/m²
- Armament
- 1 × 20 mm ShVAK cannon, with 150 rounds; 2 × 12.7 mm Berezin UBS machine guns with 170 rpg
- Built
- 4,848
Where the bar is lying
NW EuropeSpitfire IX restores parity
Eastern FrontLocally variable all year
Mediterranean
PacificHellcat and the Thach Weave
XI
1944
Escort, and a change of orders
Edge — Allies, decisively
Two changes, one mechanical and one administrative. The drop tank gave the escort the range to reach Berlin; then Doolittle released the escorts to hunt rather than nurse the bomber stream, which turned escort into a deliberate attrition campaign against the German fighter force. Behind both: Allied pilots reaching squadrons with 300-plus hours against German replacements with well under a hundred.
- Crew
- 1
- Engine
- Nakajima Homare Model Ha-45-21 (or Models 11, 12, 21, 23 or 25) — 18-cylinder air-cooled radial piston engine
- Power
- 2,041 hp
- Max speed
- 687 km/h
- Ceiling
- 11,826 m
- Climb
- 21.8 m/s
- Range
- 2,168 km
- Wingspan
- 11.24 m
- Length
- 9.92 m
- Wing area
- 21.0 m²
- Empty wt
- 2,660 kg
- Loaded wt
- 3,602 kg
- Wing loading
- 171.5 kg/m²
- Armament
- 2 × 12.7 mm Ho-103 machine guns in nose, 350 rounds/gun; 2 × 20 mm Ho-5 cannon in wings, 150 shells/cannon; 2 × 250 kg bombs; 2× 200 L (usgal) drop tanks
- Built
- 3,514
- Crew
- 1
- Engine
- Packard (Rolls-Royce) V-1650-7 Merlin — 12-cylinder liquid cooled engine
- Power
- 1,490 hp
- Max speed
- 708 km/h
- Ceiling
- 12,771 m
- Climb
- 16.3 m/s
- Range
- 2,655 km
- Wingspan
- 11.28 m
- Length
- 9.83 m
- Wing area
- 21.8 m²
- Empty wt
- 3,463 kg
- Loaded wt
- 5,490 kg
- Wing loading
- 251.8 kg/m²
- Armament
- 6 × .50 caliber (12.7mm) AN/M2 Browning machine guns with 1,840 total rounds (380 rounds for each on the inboard pair and 270 rounds for each of the outer two pair)
- Built
- 15,686
- Crew
- 1
- Engine
- Pratt & Whitney R-2800-59 — 18-cylinder air-cooled radial piston engine
- Power
- 2,000 hp
- Max speed
- 715 km/h
- Ceiling
- 12,802 m
- Climb
- 16.2 m/s
- Range
- 1,658 km
- Wingspan
- 12.42 m
- Length
- 11.00 m
- Wing area
- 27.9 m²
- Empty wt
- 4,536 kg
- Loaded wt
- 6,001 kg
- Wing loading
- 215.1 kg/m²
- Armament
- 8 × .50 in (mm) M2 Browning machine guns with 425 rounds per gun (3400 rounds total) Up to 2500 lb of bombs; 10 × 5 in HVAR unguided rockets
- Built
- 15,636
- Crew
- 1
- Engine
- Pratt & Whitney R-2800-18W — radial engine
- Power
- 2,380 hp
- Max speed
- 717 km/h
- Ceiling
- 12,649 m
- Climb
- 22.1 m/s
- Range
- 528 km
- Wingspan
- 12.50 m
- Length
- 10.26 m
- Wing area
- 29.2 m²
- Empty wt
- 4,238 kg
- Loaded wt
- 6,654 kg
- Wing loading
- 228.1 kg/m²
- Armament
- 6 × 0.50 in (12.7 mm) M2 Browning machine guns 375-400 rounds per gun
- Built
- More than 12,571
Where the bar is lying
NW EuropeLuftwaffe fighter arm broken over Germany
Eastern FrontYak and La regiments hold the front
Mediterranean
PacificMarianas Turkey Shoot, June 1944
XII
mid 1944 – May 1945
Jets, too late
Edge — Allies, absolutely
The clearest technical lead of the entire war belonged to the side losing it. The Me 262 was faster than anything opposing it and could not be exploited: the oil campaign took the fuel, dispersal took the build quality, and the Jumo 004's twenty-five-hour turbine life took the rest. This is the shape of the last era of the First World War repeated exactly — a superb fighter, and no means left to push the pendulum with it.
- Crew
- 1
- Engine
- Junkers Jumo 004B-1 — axial-flow turbojet engines
- Thrust
- 2 × 8.8 kN
- Max speed
- 900 km/h
- Ceiling
- 11,450 m
- Climb
- 20.0 m/s
- Range
- 1,050 km
- Wingspan
- 12.60 m
- Length
- 10.60 m
- Wing area
- 21.7 m²
- Empty wt
- 3,795 kg
- Loaded wt
- 6,473 kg
- Wing loading
- 298.3 kg/m²
- Armament
- 4 × 30 mm MK 108 cannon
- Built
- 1,430
- Crew
- 1
- Engine
- Hellmuth Walter Kommanditgesellschaft HWK 109-509A-2 — bi-propellant liquid-fuelled rocket motor
- Thrust
- 14.7 kN
- Max speed
- 960 km/h
- Ceiling
- 12,000 m
- Climb
- 81.3 m/s
- Endurance
- about 7.5 minutes powered
- Wingspan
- 9.30 m
- Length
- 5.70 m
- Wing area
- 19.6 m²
- Empty wt
- 1,905 kg
- Loaded wt
- 4,309 kg
- Wing loading
- 219.8 kg/m²
- Armament
- 2 × 30 mm Rheinmetall Borsig MK 108 cannon with 60 rpg
- Built
- ~370
- Crew
- 1
- Engine
- Napier Sabre IIB — H-24 liquid-cooled sleeve-valve piston engine
- Power
- 2,420 hp
- Max speed
- 700 km/h
- Ceiling
- 11,125 m
- Climb
- 12.7 m/s
- Range
- 1,190 km
- Wingspan
- 12.50 m
- Length
- 10.26 m
- Wing area
- 28.1 m²
- Empty wt
- 4,082 kg
- Loaded wt
- 5,171 kg
- Wing loading
- 184.0 kg/m²
- Armament
- 4 × 20 mm Hispano Mk II cannon
- Built
- 1,702
- Crew
- 1
- Engine
- Napier Sabre IIA, IIB or IIC — H-24 liquid-cooled sleeve-valve piston engine
- Power
- 2,180 hp
- Max speed
- 679 km/h
- Ceiling
- 9,693 m
- Climb
- 13.9 m/s
- Range
- 821 km
- Wingspan
- 12.67 m
- Length
- 9.74 m
- Wing area
- 25.9 m²
- Empty wt
- 4,010 kg
- Loaded wt
- 5,171 kg
- Wing loading
- 199.7 kg/m²
- Armament
- 4 × 20 mm Hispano Mk II cannon
- Built
- 3,317
- Crew
- Two: pilot, bomb aim
- Engine
- Rolls-Royce Merlin — V-12 liquid-cooled piston engine
- Power
- 2 × 1,710 hp
- Max speed
- 668 km/h
- Ceiling
- 11,278 m
- Climb
- 14.5 m/s
- Range
- 2,092 km
- Wingspan
- 16.51 m
- Length
- 13.56 m
- Wing area
- 42.2 m²
- Empty wt
- 6,486 kg
- Loaded wt
- 8,210 kg
- Wing loading
- 194.5 kg/m²
- Armament
- 4 × 7.7 mm Browning machine guns, 4 × 20 mm Hispano cannons
- Built
- 7,781
- Crew
- 1
- Engine
- Shvetsov ASh-82FN — 14-cylinder, two-row, air-cooled radial
- Power
- 1,851 hp
- Max speed
- 661 km/h
- Ceiling
- 10,450 m
- Climb
- 15.7 m/s
- Range
- 665 km
- Wingspan
- 9.80 m
- Length
- 8.60 m
- Wing area
- 17.6 m²
- Empty wt
- 2,638 kg
- Loaded wt
- 3,315 kg
- Wing loading
- 188.5 kg/m²
- Armament
- 2 × cowl-mounted 20 mm ShVAK cannons with 200 rounds per gun or; 3 × cowl-mounted 20 mm Berezin B-20 cannons with 100 rounds per gun
- Built
- 5,753 (+ 582 trainers)
- Crew
- 1
- Engine
- Rolls-Royce Derwent 8 — centrifugal flow turbojet engine
- Thrust
- 2 × 16.0 kN
- Max speed
- 966 km/h
- Ceiling
- 13,106 m
- Climb
- 35.6 m/s
- Range
- 966 km
- Wingspan
- 11.33 m
- Length
- 13.59 m
- Wing area
- 32.5 m²
- Empty wt
- 4,846 kg
- Loaded wt
- 7,121 kg
- Wing loading
- 219.1 kg/m²
- Armament
- 4 × 20 mm Hispano MkV cannon
- Built
- 3,947
Where the bar is lying
NW Europe
Eastern Front
Mediterranean
Pacific
XIII
1945 – 1948
Straight wings, borrowed research
Edge — West, nominally
Every power read the same captured German swept-wing and axial-compressor work at the same time. The straight-wing first generation went into service anyway because it could be built now. The consequential decision of the period was commercial: Britain sold Rolls-Royce Nene engines to the Soviet Union in 1946, and got the MiG-15 back four years later.
- Crew
- 1
- Engine
- RD-20 — axial-flow turbojet engines
- Thrust
- 2 × 7.8 kN
- Max speed
- 864 km/h
- Ceiling
- 13,000 m
- Climb
- 22.0 m/s
- Range
- 800 km
- Wingspan
- 10.00 m
- Length
- 9.75 m
- Wing area
- 18.2 m²
- Empty wt
- 3,283 kg
- Loaded wt
- 4,860 kg
- Wing loading
- 267.0 kg/m²
- Armament
- 1 × 37 mm Nudelman N-37 autocannon extending from nose intake divider ; 2 × 23 mm Nudelman-Suranov NS-23 autocannon extending from undersides of nose intake
- Built
- 610
- Crew
- 1
- Engine
- de Havilland Goblin 3 — centrifugal-flow turbojet engine
- Thrust
- 14.9 kN
- Max speed
- 882 km/h
- Ceiling
- 13,045 m
- Climb
- 24.4 m/s
- Range
- 1,963 km
- Wingspan
- 11.58 m
- Length
- 9.37 m
- Wing area
- 24.3 m²
- Empty wt
- 3,304 kg
- Loaded wt
- 5,620 kg
- Wing loading
- 231.3 kg/m²
- Armament
- 4 × 20 mm (0.79 in) Hispano Mk.V cannon with 600 rounds total (150 rounds per gun)
- Built
- 3,268
- Crew
- 1
- Engine
- Allison J33-A-35 — centrifugal compressor turbojet
- Thrust
- 20.5 kN
- Max speed
- 956 km/h
- Ceiling
- 14,265 m
- Climb
- 34.9 m/s
- Range
- 1,328 km
- Wingspan
- 11.81 m
- Length
- 10.49 m
- Wing area
- 22.1 m²
- Empty wt
- 3,819 kg
- Loaded wt
- 5,534 kg
- Wing loading
- 250.4 kg/m²
- Armament
- 6 × 0.50 in (12.7mm) M3 Browning machine guns (300 rpg)
- Built
- 1,715
- Crew
- 1
- Engine
- Allison J35-A-29 — turbojet engine
- Thrust
- 24.9 kN
- Max speed
- 1,001 km/h
- Ceiling
- 12,344 m
- Climb
- 7.9 min to 35000 ft
- Range
- 1,078 km
- Wingspan
- 11.10 m
- Length
- 11.61 m
- Wing area
- 24.2 m²
- Empty wt
- 5,033 kg
- Loaded wt
- 8,457 kg
- Wing loading
- 349.5 kg/m²
- Armament
- 6 × .50 in (12.7 mm) M3 Browning machine guns, 300 rounds per gun
- Built
- 7,524
XIV
1949 – 1950
The swept wing, and the MiG shock
Edge — USSR
Sweeping the wing reduces the airflow velocity across it, delaying the transonic drag rise and letting the aeroplane work much closer to Mach 1. The MiG-15 put a 35° wing on a light airframe around a copied Nene, and over Korea it out-climbed and out-ceilinged everything the UN had. It made the B-29 obsolete in a fortnight.
- Crew
- 1
- Engine
- Klimov VK-1 — centrifugal-flow turbojet
- Thrust
- 26.5 kN
- Max speed
- 1,076 km/h
- Ceiling
- 15,500 m
- Climb
- 51.2 m/s
- Range
- 2,520 km
- Wingspan
- 10.09 m
- Length
- 10.10 m
- Wing area
- 20.6 m²
- Empty wt
- 3,681 kg
- Loaded wt
- 5,044 kg
- Wing loading
- 244.9 kg/m²
- Armament
- 2 × 23 mm Nudelman-Rikhter NR-23 autocannon in the lower left fuselage (80 rounds per gun, 160 rounds total); 1 × 37 mm Nudelman N-37 autocannon in the lower right fuselage (40 rounds total)
- Built
- 13,130 in the USSR + at least 4,180 under license
- Crew
- 1
- Engine
- Pratt & Whitney J48-P-6A — turbojet
- Thrust
- 27.8 kN
- Max speed
- 932 km/h
- Ceiling
- 13,045 m
- Climb
- 25.9 m/s
- Range
- 2,092 km
- Wingspan
- 11.58 m
- Length
- 11.84 m
- Wing area
- 23.2 m²
- Empty wt
- 4,603 kg
- Loaded wt
- 8,492 kg
- Wing loading
- 366.0 kg/m²
- Armament
- 4 × 20 mm (0.79 in) AN/M3 cannon, 760 rounds total
- Built
- 1,385
- Crew
- 1
- Engine
- Svenska Flygmotor RM2B (de Havilland Ghost) — centrifugal-flow turbojet
- Thrust
- 27.5 kN
- Max speed
- 1,060 km/h
- Ceiling
- 15,500 m
- Climb
- 32.1 m/s
- Range
- 1,100 km
- Wingspan
- 11.00 m
- Length
- 10.23 m
- Wing area
- 24.1 m²
- Empty wt
- 4,845 kg
- Loaded wt
- 8,375 kg
- Wing loading
- 346.8 kg/m²
- Armament
- 4 x 20 mm akan m/47C (license produced Hispano Mark V) autocannon with 180 rounds per gun
- Built
- 661
XV
1951 – 1953
Korea: the aircraft were close, the pilots were not
Edge — USA, on exchange ratio
The MiG climbed higher and turned better at altitude; the Sabre dived faster and rolled quicker. What decided it was three pieces of equipment and one demographic fact: the all-flying tail, which kept pitch authority when shockwaves made a conventional elevator useless; the radar-ranging gunsight, which computed deflection faster than a person can; the G-suit; and a large pool of combat-experienced pilots against mostly ab-initio opponents. The famous kill ratio is heavily contested and belongs in a range, not a headline.
No challengerNothing on this side set a standard the other had to answer.
- Crew
- 1
- Engine
- General Electric J47-GE-27 — turbojet engine
- Thrust
- 26.3 kN
- Max speed
- 1,106 km/h
- Ceiling
- 15,118 m
- Climb
- 45.7 m/s
- Range
- 666 km
- Wingspan
- 11.91 m
- Length
- 11.30 m
- Wing area
- 29.1 m²
- Empty wt
- 5,046 kg
- Loaded wt
- 6,894 kg
- Wing loading
- 236.9 kg/m²
- Armament
- 6 x 0.50 in (12.7 mm) M3 Browning machine guns (1,800 rounds in total)
- Built
- 9,860
XVI
1953 – 1955
Supersonic in level flight
Contested — no honest winner
The afterburner, Whitcomb's area rule and irreversible powered flight controls arrive together, and the question stops being who can turn and becomes who can accelerate. The F-100 got there first and was dangerous in the process; the Hunter and the MiG-17 were the better aeroplanes to fly; the MiG-19 matched the F-100 and beat it into squadron service in numbers. Compare the wing loadings on this row against the Sopwith Camel's 30.7 kg/m² and the whole period is visible in one figure.
- Crew
- 1
- Engine
- Klimov VK-1F — afterburning centrifugal-flow turbojet engine
- Thrust
- 26.5 kN
- Max speed
- 1,100 km/h
- Ceiling
- 16,600 m
- Climb
- 65.0 m/s
- Range
- 2,020 km
- Wingspan
- 9.63 m
- Length
- 11.26 m
- Wing area
- 22.6 m²
- Empty wt
- 3,919 kg
- Loaded wt
- 5,340 kg
- Wing loading
- 236.3 kg/m²
- Armament
- 2 × 23 mm Nudelman-Rikhter NR-23 autocannon (80 rounds per gun, 160 rounds total); 1 × 37 mm Nudelman N-37 autocannon (40 rounds total)
- Built
- 10,649 including Polish, Czech and Chinese variants
- Crew
- 1
- Engine
- Tumansky RD-9B — afterburning turbojet engines
- Thrust
- 2 × 25.5 kN
- Max speed
- 1,452 km/h
- Ceiling
- 17,500 m
- Climb
- 177.8 m/s
- Range
- 1,390 km
- Wingspan
- 9.00 m
- Length
- 12.54 m
- Wing area
- 25.0 m²
- Empty wt
- 5,172 kg
- Loaded wt
- 7,560 kg
- Wing loading
- 302.4 kg/m²
- Armament
- 3 × 30 mm Nudelman-Rikhter NR-30 autocannon (75 rounds for wing-root guns, 55 rounds for the fuselage gun)
- Built
- 2,172 (excluding production in Czechoslovakia and China)
- Crew
- 1
- Engine
- Pratt & Whitney J57-P-21/21A — afterburning turbojet engine
- Thrust
- 45.4 kN
- Max speed
- 1,487 km/h
- Ceiling
- 15,240 m
- Climb
- 113.8 m/s
- Range
- 3,211 km
- Wingspan
- 11.81 m
- Length
- 15.24 m
- Wing area
- 37.2 m²
- Empty wt
- 9,525 kg
- Loaded wt
- 13,085 kg
- Wing loading
- 351.7 kg/m²
- Armament
- 4× 20 mm (0.787 in) M39A1 revolver cannon each with 200 rounds per gun
- Built
- 2,294
- Crew
- 1
- Engine
- Rolls-Royce Avon 207 — turbojet engine
- Thrust
- 45.1 kN
- Max speed
- 1,003 km/h
- Ceiling
- 15,240 m
- Climb
- 87.4 m/s
- Range
- 620 km
- Wingspan
- 10.26 m
- Length
- 13.98 m
- Wing area
- 32.4 m²
- Empty wt
- 6,406 kg
- Loaded wt
- 8,051 kg
- Wing loading
- 248.5 kg/m²
- Armament
- 4× 30 mm caliber ADEN cannon in a removable gun pack with 150 rpg
- Built
- 1,972