Electric Aircraft Corporation Electra 1

From Wikipedia, the free encyclopedia

Electra 1
Type Electric aircraft engine
National origin United States
Manufacturer Electric Aircraft Corporation
Major applications ultralight trikes

The Electric Aircraft Corporation Electra 1 is an American electric motor for powering electric aircraft, designed and produced by Electric Aircraft Corporation of Cliffside Park, New Jersey.[1]

The engine is normally sold in a package that includes "motor, electronic controller, power dial and switch, fuse, connectors, ammeter and shunt, voltmeter, custom machined propeller hub, and digital motor temperature display with probe."[2]

Design and development[]

The Electra 1 is a brushed 74 volt design producing 14 kW (19 hp). It has an 85% efficiency. The low working rpm of the engine means that it can turn a propeller at efficient speeds without the need for a reduction drive.[1]

Applications[]

Specifications (Electra 1)[]

Data from Tacke[1]

General characteristics

Components

Performance

See also[]

Related lists

References[]

  1. ^ a b c Tacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, pages 262–263. Flying Pages Europe SARL, 2015. ISSN 1368-485X
  2. ^ Electric Aircraft Corporation. "Price List". www.electraflyer.com. Retrieved 29 April 2018.

External links[]

Retrieved from ""