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Photo courtesy Falco (more images here) |
C O B R A 4 0 0 The Cobra 400 - designed by Stelio Frati - first flew on November 16, 1960. It is a two-seater jet powered by one 880lbst Turboméca Marboré II.
COBRA 480 A four seat derivative, the Cobra 480, was also designed and contruction of the first prototype was stopped in 1969 before first flight. |
COBRA 400 | COBRA 480 | |||
DIMENSIONS | ||||
Wing Span | 28 ft 6 in | 8.70 m | 29 ft 6 in | 9.0 m |
Wing area | 126.90 sqft | 11.70 m2 | 126.50 sqft | 11.75 m2 |
Aileron area (total) | 10.98 sqft | 1.02 m2 | 8.80 sqft | 0.818 m2 |
Flap area (total) | 15.50 sqft | 1.44 m2 | 21.2 sqft | 1.97 m2 |
Wing Aspect Ratio | 6.5 | 6.5 | ||
Wing section | NACA 64(3)218 | NACA 64(3)218 | ||
Wing dihedral | 6 deg | 6 deg | ||
Wing incidence | 4 deg | 4 deg | ||
Overall length | 26 ft 7 in | 8.10 m | 27 ft 3 in | 8.30 m |
Overall height | 9ft 2 in | 3.00 m | 9ft 10 in | 2.79 m |
Wheel track | 9 ft 0 1/4 in | 2.75 m | ||
Wheelbase | 10 ft 8 in | 3.25 m | ||
WEIGHTS, LOADINGS | ||||
MTOW | 3748 lb | 1700 kg | 4400 lb | 2000 kg |
Empty weight | 2425 lb | 1100 kg | 2420 lb | 1098 kg |
Max. wing loading | 29.7 lb/sq ft | 145 kg/m2 | 32.1 lb/sq ft | 171 kg/m2 |
Max fuel | 113 Imp. Gal | 515 l | 171 Imp. Gal | 780 l |
SPEEDS | ||||
Max. speed | 310 kts FL130 | 580 km/h | 330 kts FL150 | 610 km/h |
Max. cruise speed | 260 kts FL130 | 480 km/h | 275 kts FL150 | 510 km/h |
Best cruise speed (FL180) | 205 kts FL130 | 380 km/h | ||
Stall speed (power off, flaps down) (VSC) | 69 kts | 129 km/h | 69 kts | 129 km/h |
TAKE-OFF (ISA, SL) | ||||
Ground roll | 1900 ft | 580 m | ||
LANDING (ISA, SL) | ||||
Ground roll | 1400 ft | 425 m | ||
CLIMB AND ALTITUDE | ||||
Sea level | 2400 ft/min | 720 m/min | ||
Service ceiling | 28500 ft | 8700 m | ||
RANGES | ||||
Range at best cruise | 680 nm | 1250 km |
Source: Jane's All the World Aircraft.
F.1000
Last update : 21JAN05
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