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Originally posted by Vukovlad
As I understand it the 710 Km/h was achieved during test flights without armament and armor
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[SIZE=4]Morane-Saulnier MS.406[/SIZE]
[SIZE=1]OTL specs, aircraft introduced in 1932[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: one pilot
Length: 8.17 m (26 ft 9 in)
Wingspan: 10.62 m (34 ft 10 in)
Height: 2.71 m (8 ft 10 in)
Wing area: 17.10 m² (184.06 ft²)
Empty weight: 1,893 kg (4,173 lb)
Loaded weight: 2,426 kg (5,348 lb)
Powerplant: 1× Hispano-Suiza 12Y31 liquid-cooled V-12, 640 kW (860 hp)
[SIZE=3]Performance[/SIZE]
Maximum speed: 486 km/h (303 mph) at 5,000 m (16,400 ft)
Range: 1,000 km (620 mi)
Rate of climb: 13.0 m/s (2,560 ft/min)
Wing loading: 141.9 kg/m² (29.1 lb/ft²)
Power/mass: 260 W/kg (0.16 hp/lb)
[SIZE=3]Armament[/SIZE]
- 1 × 20 mm Hispano-Suiza HS.404 cannon
- 2 × 7.5 mm MAC 1934 machine guns
[SIZE=4]Morane-Saulnier MS.410[/SIZE]
[SIZE=1]Aircraft introduced in 1934[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: one pilot
Length: 8.17 m (26 ft 9 in)
Wingspan: 10.62 m (35 ft 10 in)
Height: 2.71 m (8 ft 10 in)
Wing area: 17.10 m² (184.06 ft²)
Empty weight: 1923 kg (4240 lb)
Loaded weight: 2581 kg (5690 lb)
Powerplant: 1× Hispano-Suiza 12Y31 liquid-cooled V-12, 640 kW (860 hp)
[SIZE=3]Performance[/SIZE]
Maximum speed: 316 mph (509 km/h)
Range: 1,100 km (683.5 mi)
Rate of climb: 13.0 m/s (2,560 ft/min)
Wing loading: 141.9 kg/m² (29.1 lb/ft²)
Power/mass: 260 W/kg (0.16 hp/lb)
[SIZE=3]Armament[/SIZE]
- 1 × 20 mm Hispano-Suiza HS.404 cannon
- 4 × 7.5 mm MAC 1934 machine guns
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[SIZE=4] Bloch MB.152C.1[/SIZE]
[SIZE=1]OTL Specs, entered service in 1935[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: one, pilot
Length: 9.10 m (29 ft 10 in)
Wingspan: 10.54 m (34 ft 7 in)
Height: 3.20 m (9 ft 11 in)
Wing area: 17.32 m² (186 ft²)
Empty weight: 2,158 kg (4,758 lb)
Loaded weight: 2,693 kg (5,937 lb)
Max takeoff weight: 2,800 kg (6,173 lb)
Powerplant: 1× Gnome-Rhône 14N-25 14-cylinder, two-row, air-cooled radial engine, 757 kW (1,030 hp)
[SIZE=3]Performance[/SIZE]
Maximum speed: 515 km/h (274 kn, 315 mph)
Range: 600 km (324 nmi, 373 mi)
Service ceiling: 10,000 m (32,810 ft)
Rate of climb: 590 m/min (1,935 ft/min)
Wing loading: 155.4 kg/m² (31.9 lb/ft²)
Power/mass: 0.29 kW/kg (0.17 hp/lb)
[SIZE=3]Armament[/SIZE]
- 2× 20 mm Hispano 404 cannons (60-round drum) and 2× 7.5 mm MAC 1934 machine guns with 675 rpg or
- 4× MAC 1934s
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[SIZE=4]Dewoitine D.520C.1[/SIZE]
[SIZE=1]OTL Aircraft, introduced 1935[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: 1
Length: 8.6 m (28 ft 3 in)
Wingspan: 10.2 m (33 ft 5S in)
Height: 2.57 m (8 ft 5 in)
Wing area: 15.87 m² (171 ft²)
Empty weight: 2,123 kg (4,680 lb)
Loaded weight: 2,677 kg (5,902 lb)
Max takeoff weight: 2,785 kg (6,140 lb)
Powerplant: 1× Hispano-Suiza 12Y-45 liquid-cooled V12 engine, 690 kW (930 hp)
[SIZE=3]Performance[/SIZE]
Maximum speed: 535 km/h (302 kn, 332 mph at 18,040 feet, 263.9 mph at sealevel)
Range: 1,250 km (675 nmi, 777 mi)
Service ceiling: 10,000 m (33,000 ft)
Rate of climb: 14.3 m/s (2,820 ft/min)
Wing loading: 167 kg/m² (34.2 lb/ft²)
Power/mass: 257 W/kg (0.156 hp/lb)
[SIZE=3]Armament[/SIZE]
- 1 × 20 mm Hispano-Suiza HS.404 (60-round drum) cannon
- 4 × 7.5 mm (0.295 in) MAC 1934 (675 rpg) machine guns
[SIZE=4]Dewoitine D.524C.1[/SIZE]
[SIZE=1]Improved D.520, introduced 1937[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: 1
Length: 8.6 m (28 ft 3 in)
Wingspan: 10.2 m (33 ft 5S in)
Height: 2.57 m (8 ft 5 in)
Wing area: 15.87 m² (171 ft²)
Empty weight: 2,123 kg (4,680 lb)
Loaded weight: 2,677 kg (5,902 lb)
Max takeoff weight: 2,785 kg (6,140 lb)
Powerplant: 1× HS 12Y89ter liquid-cooled V12 engine, 1,280hp
[SIZE=3]Performance[/SIZE]
Maximum speed: 560 km/h (302 kn, 347 mph)
Range: 1,250 km (675 nmi, 777 mi)
Service ceiling: 10,000 m (33,000 ft)
Rate of climb: 14.3 m/s (2,820 ft/min)
Wing loading: 167 kg/m² (34.2 lb/ft²)
Power/mass: 257 W/kg (0.156 hp/lb)
[SIZE=3]Armament[/SIZE]
- 1 × 20 mm Hispano-Suiza HS.404 (60-round drum) cannon
- 4 × 7.5 mm (0.295 in) MAC 1934 (675 rpg) machine guns
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[SIZE=4]Arsenal VG.33[/SIZE]
[SIZE=1]OTL specs, aircraft introduced in 1937[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: one, pilot
Length: 8.55 m (28 ft 0 in)
Wingspan: 10.8 m (35 ft 3 in)
Height: 3.31 m (10 ft 10 in)
Wing area: 150.7 m² (14 ft²)
Empty weight: 2,050 kg (4,519 lb)
Loaded weight: 2,655 kg (5,853 lb)
Powerplant: 1× Hispano-Suiza 12Y31 supercharged liquid-cooled 60° V12 engine, 641 kW (860 hp)
[SIZE=3]Performance[/SIZE]
Maximum speed: 558 km/h (301 knots, 347 mph)
Range: 1,200 km (648 nm, 720 mi)
Service ceiling: 11,000 m (36,090 ft)
[SIZE=3]Armament[/SIZE]
1 × 20 mm Hispano-Suiza HS.404 cannon
4 × 7.5 mm MAC 1934 machine guns
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[SIZE=4]Arsenal VG.36[/SIZE]
[SIZE=1]Aircraft introduced in 1939[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: one, pilot
Length: 8.55 m (28 ft 0 in)
Wingspan: 10.80 m (35 ft 5 in)
Height: 3.31 m (10 ft 10 in)
Wing area: 150.7 m² (14 ft²)
Empty weight: 2,050 kg (4,519 lb)
Loaded weight: 2,655 kg (5,853 lb)
Powerplant: 1 × Hispano-Suiza 12Y-51 supercharged liquid-cooled 60° V12 engine, (1000 hp)
[SIZE=3]Performance[/SIZE]
Maximum speed: 575 km/h (357 mph)
Range: 1,100 km (684 mi)
Service ceiling: 11,000 m (36,090 ft)
[SIZE=3]Armament[/SIZE]
1 × 20 mm Hispano-Suiza HS.404 cannon
4 × 7.5 mm MAC 1934 machine guns
[SIZE=3]Notes:[/SIZE]
- Longer-ranged variant (VG.37) also constructed; 100 license-built by Potez.
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[SIZE=4]Arsenal VG.39bis[/SIZE]
[SIZE=1]Aircraft introduced in 1940[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: one, pilot
Length: 8.75 m (29 ft 8 in)
Wingspan: 10.80 m (35 ft 5 in)
Height: 3.31 m (10 ft 10 in)
Wing area: 150.7 m² (14 ft²)
Empty weight: 2,050 kg (4,519 lb)
Loaded weight: 2,655 kg (5,853 lb)
Powerplant: 1 × Hispano-Suiza 12Z supercharged liquid-cooled 60° V12 engine, (1500 hp)
[SIZE=3]Performance[/SIZE]
Maximum speed: 625 km/h (388 mph)
Range: ?
Service ceiling: 11,000 m (36,090 ft)
[SIZE=3]Armament[/SIZE]
6 × 7.5 mm MAC 1934 machine guns
[SIZE=3]Notes[/SIZE]
The VG.39bis is the production version of the VG.39. The VG.39bis allegedly had a 1,600hp Hispano-Suiza 12Z engine with 1,600hp. The initial VG.39 had a HS-12Y89ter engine with 1,280hp and allegedly achieved the above performance figures.
Starting in 1941, all new VG.39bis are produced with a bubble canopy.
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[SIZE=4]Loire-Nieuport LN-180[/SIZE]
[SIZE=1]License-built Stampe SV.4b, license acquired 1940.[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: 1-2
Length: 6.80 m (22 ft 4 in)
Wingspan: 8.385 m (27 ft 6 in)
Height: 2.775 m (9 ft 1 in)
Wing area: 18.06 m² (194.4 ft²)
Empty weight: 520 kg (1146 lb)
Max takeoff weight: 770 kg (1697 lb)
Powerplant: 1× de Havilland Gipsy Major X or Blackburn Cirrus Major III, 145 hp (108 kW)
[SIZE=3]Performance[/SIZE]
Maximum speed: 101 knots (188 km/h)
Cruise speed: 75 knots (140 km/h)
Range: 420 km (260 statute miles)
Service ceiling: 20,000 ft (6,000 m)
[SIZE=3]Notes[/SIZE]
Also manufactured by Atelier Industriel de l'Aéronautique d'Alger and Atelier Industriel de l'Aéronautique d'Indochine
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[SIZE=4]Nord Pingouin[/SIZE]
[SIZE=1]License-built Bf108, license acquired 1940.[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: 1
Capacity: 3 passengers
Length: 8.28 m (27 ft 2 in)
Wingspan: 10.61 m (34 ft 10 in)
Height: 2.29 m (7 ft 6½ in)
Empty weight: 881 kg (1941 lb)
Gross weight: 1356 kg (2987 lb)
Powerplant: 1 × Renault 6Q 10, 179 kW (240 hp)
[SIZE=3]Performance[/SIZE]
Cruising speed: 257 km/h (160 mph)
Range: 997 km (620 miles)
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[SIZE=4]Nord Noralpha[/SIZE]
[SIZE=1]License-built and redesigned Bf108; in production late 1941ish.[/SIZE]
[SIZE=3]General characteristics[/SIZE]
Crew: 1
Capacity: 3 passengers
Length: 8.53 m (28 ft 0 in)
Wingspan: 11.48 m (37 ft 8 in)
Height: 3.25 m (10 ft 8 in)
Wing area: 17.37 m² (187 ft²)
Empty weight: 948 kg (2,090 lb)
Gross weight: 1,645 kg (3,627 lb)
Powerplant: 1 × Renault 6Q 10 inline piston engine, 179 kW (240 hp)
[SIZE=3]Performance[/SIZE]
Maximum speed: 305 km/h (189 mph)
Range: 1,200 km (745 miles)
Service ceiling: 5,900 m (19,355 ft)
[SIZE=3]Notes[/SIZE]
Historical Noralpha with French engine and tricycle landing gear.
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