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Specifications: Sud-Est SE. 2410 Grognard, SE. 2415 Grognard II (SE.2415 data corresponding in brackets)
Usage: Low-attack aircraft
Engine: two Rolls Royce RB.41 Nene with single-stage radial compressor and 9 combustion chambers
Stand thrust: 2,262 kp (22.2 kN)
Continuous power: 1,820 kp (17.84 kN) in 8,000 m
First flight Sud-Est SE. 2410: April 30, 1950
First flight SE. 2415: February 14, 1951
Built: 1949 (1951)
Crew: 1 man (2 men)
Dimensions:
Wingspan: 13.58 m (13.58 m), Length: 15.44 m (16.84 m), Hight : 5.70 m (5.20 m)
largest wing chord: 4.95 m (3.60 m), largest wing thickness: 0.58 m (0.48 m)
largest hull height: 2.72 m (2.68m), largest hull width: 2.23 m (2.02m)
Wingspan side tail: 6.98 m (6.00 m), Track gauge: 3.08 m (2.70 m), Wheelbase: 5.35 m (4.60 m)
Wing area: 46.14 m2 (44.23 m2), Sweep back angle of wing front edge: 47° (32°), Tail: 35° (37°)
Empty mass: 11,117 kg (11,512 kg), Starting mass normal: 15,820 kg (17,050 kg), Maximum take-off mass: 17,060 kg (18,160 kg)
Tank capacity: 2,400 litres (2,600 litres), Area load: 369.74 kg/m2 (410.58 m2), Power load: 3.41 kg/hp (4.64 kg/kW)
Services:
Top speed near the ground: 1,038 km/h (960 km/h), Top speed in 8,000 m: 1060 km/h (982 km/h)
Cruising speed in 8,000 m: 880 km/h (880 km/h), Take off speed: 240 km/h (220 km/h), Landing speed: 180 km/h (180 km/h)
Ceiling: 9,600 m (9,000m)
Climbing rate: 47.8 m/s (44 m/s), Climbing time at 1,000 m: 22 sec (25 sec), Climbing time at 8,000 m: 4.0 min (4.5 min)
Range normal: 1.450 km (1,580 km), Maximum range: 1,720 km (1,880 km), Flight duration: 2 h (2.25 h)
Take off run: 920 m
Armament: two 30 mm defA 552 machine guns with 100 rounds each
32 unguided 2 inch matra missiles and four steerable air-to-air missiles Matra T10
Bomb load: max. 1000 kg