macroeconomics-Nexaer LS1

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University of Maryland, University College *

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201 7982

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Industrial Engineering

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Oct 30, 2023

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pdf

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Nexaer LS1 The Nexaer LS1 is an American light-sport aircraft, under evolution past Nexaer of Peyton, Colorado, n flown along 16 October 2006. The aircraft is intended to be supplied arsenic a consummate ready-to-fly-aircraft. Designing and evolution The LS1 was unintentional to follow with the US light-sport aircraft rules. It features a cantilever low-wing, a two-seats-in-side-by-side constellation enclosed cockpit, rigid tricycle landing pitch and a single locomotive in tractor configuration. The LS1 has a distinctively curving fuselage.The aircraft is made from composites. Its 29.5 foot (9.0 m) couple wing has an country of 124 sq ft (11.5 m2) and for simmpleness has no flaps. Touchstone engines useable are the Hundred hp (75 kW) Rotax 912ULS, 85 hp (63 kW) Jabiru 2200, 120 hp (89 kW) Jabiru 3300, 100 hp (75 kW) Continental O-200 and the 108 horsepower (81 kW) Lycoming O-235 four-stroke powerplants. The cockpit is 54 in (137 cm) in width. Specifications (LS1) Data from Bayerl and NexaerGeneral characteristics Crew: one Capacity: 1 passenger Length: 23 foot Three in (7.09 m) Wingspan: 29 foot Six in (8.99 m) Height: Seven ft 10 in (2.39 m) Wing area: 124 sq foot (11.5 m2) Empty weight: 750 pound (340 kg) Gross weight: 1,320 lb (599 kg) Fuel capacity: 27 U.S. gallons (100 L; 22 rapscallion gal) Powerplant: 1 × Jabiru 2200 4 cylinder, air-cooled, quaternary shot aircraft engine, 85 horsepower (63 kW)Performance Maximum speed: 140 mph (220 km/h, 120 kn) Cruise speed: 120 mph (200 km/h, 110 kn) Stall speed: Fifty-one mph (82 km/h, 44 kn) g limits: +4.5/-2.0
Wing loading: 10.6 lb/sq ft (52 kg/m2) References Outside, links Official website
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