| In June 1946, the Service Technique Aeronautique
issued a preliminary requirement for a shipboard
fighter armed with three 20mm or 30mm cannon and
capable of carrying two 500kg bombs or eight
90mm rockets. Responding to this requirement, the
SNCA du Nord tendered the Nord 2200, designed by a
team led by Messrs Coroller, Dupin and Buret, in competition
with the Aerocentre NC 1080 and the Arsenal
VG 90. Powered by a 2268kg Hispano-
Suiza Nene 102 turbojet and featuring a 24° sweptback
laminar-flow wing with large Fowler-type flaps,
the Nord 2200 was first flown on 16 December 1949, and
was fitted with neither wing folding nor armament. On
24 June 1950, the sole prototype was damaged and the
opportunity was taken to fit a servo control system, introduce
redesigned and larger vertical tail surfaces,
and make provision for an AI radar scanner over the
engine air intake. Flight testing was resumed on 24
May 1951, but in 1952 the decision was taken by the
Aeronavale to adopt the de Havilland Sea Venom to
meet its shipboard fighter requirement. Nevertheless, flight testing of the Nord 2200 continued until June
1954.
| A three-view drawing (1667 x 1103) |
WEIGHTS |
Take-off weight | 7890 kg | 17395 lb |
Empty weight | 4830 kg | 10648 lb |
DIMENSIONS |
Wingspan | 12.00 m | 39 ft 4 in |
Length | 13.90 m | 46 ft 7 in |
Height | 4.80 m | 16 ft 9 in |
Wing area | 31.60 m2 | 340.14 sq ft |
PERFORMANCE |
Max. speed | 936 km/h | 582 mph |
bingshuya, 20.06.2011 06:07 Sea Venom to meet its shipboard fighter requirement. Nevertheless, flight testing of the Nord 2200 continued until June 1954. reply |
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