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The aircraft has a standard empty weight of 245 lb (111 kg). [1] The B-10's fuselage is made from aluminum tubing while the wing has a birch plywood D-cell leading edge and foam ribs, covered with Dacron sailcloth or doped aircraft fabric. The tailless wing is common to all three variants. [2] It is of tapered and lightly-swept form, employing ...
Data from Cliche and Virtual Ultralight Museum General characteristics Crew: one Length: 15 ft 0 in (4.57 m) Upper wingspan: 24 ft 0 in (7.32 m) Lower wingspan: 20 ft 4 in (6.20 m) Height: 6 ft 0 in (1.83 m) Wing area: 160 sq ft (15 m 2) Empty weight: 218 lb (99 kg) Gross weight: 415 lb (188 kg) Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal) Powerplant: 1 × Cuyuna 430R, 30 hp (22 kW ...
All members of the series are made from bolted-together aluminum tubing, ... 10.20 m (33 ft 6 in) Height ... Aspect ratio: 5.4:1; Empty weight: 59 kg (130 lb) wing ...
2195 aluminium alloy is an alloy in the wrought aluminium-copper family (2000 or 2xxx series). It is one of the Weldalite family of Aluminium–lithium alloys. [1] It is one of the most complex grades in the 2000 series, with at least 91.9% aluminium by weight. 2195 aluminium can be alternately referred to by the UNS designation A92195.
The aluminum structure wing, ... The aircraft was designed for a maximum gross weight of 1,500 lb (680 kg) in the utility category, but is limited to 1,320 lb (600 kg ...
It is also known as the stiffness to weight ratio or specific ... (10 3 m 5 kg −1 s ... Balsa, low density (4.4 lb/ft 3) [25] 1.41: 0.071: 20: 280: 3,940: Tungsten ...