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The Henderson Longster is a conventional landing gear equipped, wire braced parasol wing aircraft. Aeronautical designer Ivan Diggs designed a new 30 ft wing for the Longster. [1] The wire bracing is supported by a central cabane post located over a 1 U.S. gallon (3.8 L; 0.83 imp gal) above-wing fuel tank. The fuselage is steel tubing.
A model of the Transonic Truss-Braced Wing aircraft in a wind tunnel at NASA's Ames Research Center. By early 2019, following extensive wind tunnel testing at NASA Ames Research Center, an optimized truss and more sweep for the 170 ft (52 m) span wing allowed flying higher and faster, up from Mach 0.70–0.75 to Mach 0.80 like current jetliners. [3]
"Electric aircraft generates buzz at Oshkosh air show". Chicago Tribune. August 1, 2010. "Air show examines hybrid airliners". United Press. Aug 2, 2010. "NASA, Boeing Test Low-Drag Truss-Braced Wing Concept: High-aspect-ratio, truss-braced wing promises marked fuel savings". Aviation Week & Space Technology. Aviation Week Network. January 27, 2014
The aircraft is mainly built from sheet aluminium, with the tail and rear sections of the wings fabric covered to save weight. [1] [3] The wings are constructed using a "D" cell, with stamped ribs and a single wing strut. The standard wing span on the Maverick is 29 ft 6 in (8.99 m), but an optional wing extension is available to increase the ...
The aircraft has a typical empty weight of 985 lb (447 kg) and a gross weight of 1,800 lb (820 kg), giving a useful load of 815 lb (370 kg). With full fuel of 31.75 U.S. gallons (120.2 L; 26.44 imp gal) the payload for the crew/pilot, passengers and baggage is 625 lb (283 kg).
The Low-Wing Longster is a single place, wire braced, low wing, open cockpit aircraft with conventional landing gear. The lower wing wire bracing is connected to the landing gear. The root wing ribs are oversized to create a smooth wing to fuselage fillet. The aircraft was the last in a series of homebuilt aircraft designs from Les Long.
Its 33.1 ft (10.1 m) span wing is cable braced from a single kingpost. The nose angle is 125–128° depending on VG setting, wing area is 160 sq ft (15 m 2 ) and the aspect ratio is 6.8:1. The glider empty weight is 68 lb (31 kg) and the pilot hook-in weight range is 160 to 260 lb (73 to 118 kg).
Eight aircraft were ordered by the IGN, based at Creil airfield to the north of Paris. The aircraft's wing design made it ideal for long-duration, low-speed flight, ideal for aerial photography and survey work. These machines were designated HD.34 and were fitted with an extensively glazed nose and an offset retractable nosewheel. They flew ...
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