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Dassault MD.455 Marin
The MD.455 Marin is a navalized variant of the Dassault MD.451 Ouragan II. The Marin received doubled main and nose wheels, reinforced landing gear, folding wings, and a tailhook. Some attempts were made during production to increase the aircraft's effective operating range. The final aircraft was heavier than the original Ouragan, and had a lower top speed and rate of climb.

The Marin entered service with the Aeronavale in September of 1947, re-equipping part of the fighter groups of the carriers Bucentaure and Conquérant beginning in early 1948. However, its limitation of low range meant that it could never fully replace the propeller-driven Dassault Milan. Lessons learned on the Marin, as well as the other early French jets, were eventually incorporated into the Dassault Mistral, which appeared in 1950.

General characteristics
Crew: One
Length: 10.73 m (35 ft 2 in)
Wingspan: 13.16 m (43 ft 2 in)
Height: 4.14 m (13 ft 7 in)
Wing area: 23.8 m² (256.2 ft²)
Aspect ratio: 7.3:1
Empty weight: 4,380 kg ( lb)
Loaded weight: 7,644 kg ( lb)
Max takeoff weight: 8,190 kg ( lb)
Powerplant: 1 × Rateau-Anxionnaz A.65 turbojet, 22.2 kN (4,990 lbf)

Performance
Never exceed speed: Mach 0.83
Maximum speed: 910 km/h (491 knots, 562 mph) (Mach 0.74) at sea level
Cruise speed: 725 km/h (391 knots, 450 mph)
Combat radius: 750 km (466 mi)
Ferry range: 1350 km (839 mi)
Service ceiling: 13,000 m (42,650 ft)
Rate of climb: 34 m/s (6,693 ft/min)

Armament
Guns: 4 × 23 mm DEFA revolver cannon with 125 rounds per gun
Rockets: 16× 105 mm (4.1 in) Brandt T-10 air-to-ground unguided rockets; or, 2× Matra rocket pods with 18× SNEB 68 mm rockets each
Bombs: 2,270 kg (5,000 lb) of payload on four external hardpoints, including a variety of unguided iron bombs such as 2× 454 kg (1,000 lb) bombs or 2× 458 liter (121 US gallon) napalm bombs or drop tanks for extended range.

Quoted

Dassault MD.451 Ouragan II

General characteristics
Crew: One
Length: 10.73 m (35 ft 2 in)
Wingspan: 13.16 m (43 ft 2 in)
Height: 4.14 m (13 ft 7 in)
Wing area: 23.8 m² (256.2 ft²)
Aspect ratio: 7.3:1
Empty weight: 4 142 kg (9,132 lb)
Loaded weight: 7 404 kg (16,323 lb)
Max takeoff weight: 7 900 kg (17,416 lb)
Powerplant: 1 × Rateau-Anxionnaz A.65 turbojet, 22.2 kN (4,990 lbf)

Performance
Never exceed speed: Mach 0.83
Maximum speed: 940 km/h (508 knots, 584 mph) (Mach 0.76) at sea level
Cruise speed: 750 km/h (405 knots, 465 mph)
Combat radius: 450 km (245 nm, 280 mi)
Ferry range: 920 km (500 nm, 570 mi)
Service ceiling: 13 000 m (42,650 ft)
Rate of climb: 38 m/s (7,480 ft/min)
Takeoff distance: 783 m (2,570 ft)
Landing distance: 910 m (2,985 ft)

Armament
Guns: 4 × 23 mm DEFA 501 revolver cannon with 125 rounds per gun
Rockets: 16× 105 mm (4.1 in) Brandt T-10 air-to-ground unguided rockets; or, 2× Matra rocket pods with 18× SNEB 68 mm rockets each
Bombs: 2,270 kg (5,000 lb) of payload on four external hardpoints, including a variety of unguided iron bombs such as 2× 454 kg (1,000 lb) bombs or 2× 458 liter (121 US gallon) napalm bombs or Drop tanks for extended range.