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The SB-10 is a cantilever shoulder-wing monoplane with a steel-tube structure fuselage and it used the wings from the earlier SB-9 Stratus.[1] The two crew sit in tandem in an enclosed cockpit with a Plexiglas canopy, and it is fitted with dual instrumentation.[1] The landing gear is a sprung retractable monowheel with a tail bumper.[1] The wingtips are interchangeable and two types can be fitted to give a 26m or 29m span.[1] The wing center section, its main spar and wing shells of 8m length were built using carbon fiber, a first in civil aircraft structure manufacturing.
Specifications (with 29m wing)
Data from Jane's All the World's Aircraft 1973-74[1]
General characteristics
Crew: 2
Length: 10.36 m (33 ft 11.75 in)
Wingspan: 29.00 m (95 ft 1.75 in)
Height: 2.50 m (8 ft 2.5 in)
Wing area: 22.95 m2 (247 sq ft)
Aspect ratio: 36.6
Empty weight: 577 kg (1,272 lb)
Gross weight: 897 kg (1,977 lb)
Performance
Maximum speed: 200 km/h (124 mph, 108 kn)
Stall speed: 65 km/h (40.5 mph, 35.2 kn)
g limits: +5.3
Maximum glide ratio: 53
Rate of sink: 0.41 m/s (81 ft/min)
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24 авг 2024
