Liaoning Ruixiang RX1E

The Liaoning Ruixiang RX1E is a Chinese two-seat electric aircraft, designed by the Liaoning General Aviation Academy at Shenyang Aerospace University and manufactured by the Liaoning Ruixiang General Aviation Manufacture Company Limited of Shenyang.[1]

RX1E
Role Electric aircraft
National origin China
Manufacturer Liaoning Ruixiang General Aviation Manufacture Company Limited
Introduction November 2012
Produced 2015-present
Unit cost
US$163,000 (2014)

The aircraft was first shown at the Zhuhai China Airshow, in November 2012 and in 2015 at the AERO Friedrichshafen show in Germany.[1]

Design and development

The result of a three-year development process started in June 2012, the RX1E is an electric powered, two-seat side-by-side configuration, carbon fibre composite construction aircraft with a T-tail and tricycle landing gear and is one of the first electric airplanes in production. The company said in April 2015 that they had 28 orders for the design.[1][2][3]

The manufacturer claims that the aircraft conforms to US Light-sport Aircraft requirements and has a Type Design Approval from the Civil Aviation Administration of China, issued in 2015. As of September 2016 it does not appear on the US Federal Aviation Administration list of approved LSAs and, in fact, the category excludes electric-powered aircraft and requires a single reciprocating engine.[1][4][5]

The first two customer aircraft were delivered in June 2015. The launch customer was the Liaoning Ruixiang General Aviation Co., which will employ the aircraft in the flight training role.[6]

An improved version, the RX1E-A, was first flown in November 2017 and features a two-hour endurance and a new ballistic parachute design. The original RX1E has a 45-minute endurance.[7]

Specifications (RX1E)

Data from Tacke[1]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 6.58 m (21 ft 7 in)
  • Wingspan: 14.5 m (47 ft 7 in)
  • Height: 2.45 m (8 ft 0 in)
  • Wing area: 12 m2 (130 sq ft)
  • Empty weight: 270 kg (595 lb)
  • Gross weight: 500 kg (1,102 lb)
  • Propellers: 2-bladed wooden fixed pitch

Performance

  • Cruise speed: 110 km/h (68 mph, 59 kn)
  • Stall speed: 73 km/h (45 mph, 39 kn)
  • Never exceed speed: 160 km/h (99 mph, 86 kn)
  • Endurance: 60 minutes
  • Service ceiling: 1,400 m (4,600 ft)
  • Wing loading: 41.7 kg/m2 (8.5 lb/sq ft)
gollark: NO!
gollark: Basically any sane general-purpose language can run an HTTP server.
gollark: ... yes, obviously?
gollark: What?
gollark: Also Rust on a few things.

See also
  • Aero Electric Sun Flyer
  • Pipistrel Alpha Electro

References
  1. Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 15 and 66. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. "Report: China To Start Electric Airplane Production". AVweb. Retrieved 23 June 2015.
  3. Grady, Mary (16 April 2015). "E-Flight Takes Center Stage At Aero". avweb.com. Aviation Publishing Group. Retrieved 17 April 2015.
  4. Federal Aviation Administration (26 September 2016). "SLSA Make/Model Directory". Retrieved 13 December 2016.
  5. Experimental Aircraft Association (2015). "About the Aircraft". Retrieved 13 December 2016.
  6. "China Delivers First Electric Airplanes". AVweb. Retrieved 23 June 2015.
  7. Grady, Mary (2 November 2017). "Advances For New Flight Technologies". AVweb. Retrieved 6 November 2017.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.