| Flown for the first time in November 1939, paradoxically
some six months prior to the CR 760, the CR 770
employed an essentially similar airframe and armament,
but was powered by a Renault 62616-cylinder inverted-
Vee air-cooled engine rated at 800hp at 4000m. Ten minutes after taking off for the first time,
the CR 770 suffered a broken crankshaft, and, before a
replacement power plant could be delivered to Guyancourt
where the test programme was being conducted,
the prototype had to be destroyed to avoid capture by
the Wehrmacht. The ultimate development of Marcel
Riffard's series of lightweight fighters, the CR 780, was
to have had a 500hp Renault 468 12-cylinder engine
driving contra-rotating three-bladed propellers and an
armament of two 20mm HS 404 cannon and two
7.5mm MAC 1934 M 39 machine guns, but this progressed
no further than the design study stage.
MODEL | CR 770 (performance data estim |
WEIGHTS |
Take-off weight | 2248 kg | 4956 lb |
Empty weight | 1740 kg | 3836 lb |
DIMENSIONS |
Wingspan | 8.68 m | 29 ft 6 in |
Length | 9.90 m | 33 ft 6 in |
Height | 2.92 m | 10 ft 7 in |
Wing area | 12.50 m2 | 134.55 sq ft |
PERFORMANCE |
Max. speed | 590 km/h | 367 mph |
Range | 1 500 km | 932 miles |
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