The Nexaer LS1 is an American light-sport aircraft, under development by Nexaer of Peyton, Colorado, first flown on 16 October 2006. The aircraft is intended to be supplied as a complete ready-to-fly-aircraft.[1][2]
The aircraft is made from composites. Its 29.5 ft (9.0 m) span wing has an area of 124 sq ft (11.5 m2) and for simplicity has no flaps. Standard engines available are the 100 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 hp (81 kW) Lycoming O-235four-stroke powerplants. The cockpit is 54 in (137 cm) in width.[1]
^ abcdBayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 66. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
^30dps. "news | First Flight". Nexaer. Retrieved August 9, 2012.
^30dps. "the plane | Specifications". Nexaer. Retrieved August 9, 2012.
External links
Official website
April 24, 2023
nexaer, american, light, sport, aircraft, under, development, nexaer, peyton, colorado, first, flown, october, 2006, aircraft, intended, supplied, complete, ready, aircraft, ls1role, light, sport, aircraftnational, origin, united, statesmanufacturer, nexaerfir. The Nexaer LS1 is an American light sport aircraft under development by Nexaer of Peyton Colorado first flown on 16 October 2006 The aircraft is intended to be supplied as a complete ready to fly aircraft 1 2 LS1Role Light sport aircraftNational origin United StatesManufacturer NexaerFirst flight 16 October 2006Status Under development 2012 Number built One Contents 1 Design and development 2 Specifications LS1 3 References 4 External linksDesign and development EditThe LS1 was designed to comply with the US light sport aircraft rules It features a cantilever low wing a two seats in side by side configuration enclosed cockpit fixed tricycle landing gear and a single engine in tractor configuration The LS1 has a distinctively curved fuselage 1 The aircraft is made from composites Its 29 5 ft 9 0 m span wing has an area of 124 sq ft 11 5 m2 and for simplicity has no flaps Standard engines available are the 100 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 hp 81 kW Lycoming O 235 four stroke powerplants The cockpit is 54 in 137 cm in width 1 Specifications LS1 EditData from Bayerl and Nexaer 1 3 General characteristicsCrew one Capacity one passenger Length 23 ft 3 in 7 09 m Wingspan 29 ft 6 in 8 99 m Height 7 ft 10 in 2 39 m Wing area 124 sq ft 11 5 m2 Empty weight 750 lb 340 kg Gross weight 1 320 lb 599 kg Fuel capacity 27 U S gallons 100 L 22 imp gal Powerplant 1 Jabiru 2200 four cylinder air cooled four stroke aircraft engine 85 hp 63 kW Performance Maximum speed 140 mph 220 km h 120 kn Cruise speed 120 mph 200 km h 110 kn Stall speed 51 mph 82 km h 44 kn g limits 4 5 2 0 Wing loading 10 6 lb sq ft 52 kg m2 References Edit a b c d Bayerl Robby Martin Berkemeier et al World Directory of Leisure Aviation 2011 12 page 66 WDLA UK Lancaster UK 2011 ISSN 1368 485X 30dps news First Flight Nexaer Retrieved August 9 2012 30dps the plane Specifications Nexaer Retrieved August 9 2012 External links EditOfficial website Retrieved from https en wikipedia org w index php title Nexaer LS1 amp oldid 1111742569, wikipedia, wiki, book, books, library,
