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Societe Nationale de Constructions Aeronautiques Du Sud Est S.E.2415 Grognard II

se2415


A second prototype, the SE.2415 Grognard II, flew in February 1945. A two-seater with wings swept at 32 degrees, it was damaged in a belly landing. Both designs suffered from flutter-induced problems. The definitive production version would have been the SE.2418, which was to have been powered by Rolls-Royce Tay turbojets, but the SO Vautour was selected to meet the Armee de l'Air's ground-attack requirement instead.

SE.2415-08
Engine: 1 x 2400kg Rolls-Royce Nene 102 turbojet
Max take-off weight: 18000 kg / 39683 lb
Empty weight: 11312 kg / 24939 lb
Wingspan: 13.58 m / 45 ft 7 in
Length: 16.84 m / 55 ft 3 in
Height: 5.20 m / 17 ft 1 in
Wing area: 44.23 sq.m / 476.09 sq ft
Max. speed: 960 km/h / 597 mph
Cruise speed: 880 km/h / 547 mph

se2145-ld
Sud-Est S.E.2415 Grognard II


 

 


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