Mosler_Red_82X

Mosler Red 82X

Mosler Red 82X

Add article description

The Mosler Red 82X is an experimental four cylinder, four stroke engine developed as a low cost replacement for older aircraft.

Quick Facts Type, Manufacturer ...

Design and development

A Red 82X was tested in April 1992 on a Luscombe 8A certified in the experimental-exhibition category.[1]

Variants

Red 82X
Red 82DX
Dual ignition
Red 82LB
No ignition packaged

Specifications (Red 82X)

General characteristics

  • Type: 4-cylinder, air-cooled, horizontally opposed engine
  • Bore: 94 mm
  • Stroke: 78 mm
  • Displacement: 2,165 cc
  • Length: 24 in
  • Width: 30 in
  • Height: 18 in
  • Dry weight: 182 lb

Components

  • Valvetrain: 1 inlet and 1 exhaust valve per cylinder Hydraulic lifters
  • Cooling system: Air

Performance

  • Power output: 82 hp at 3,200 rpm

See also

Related lists

References

  1. [1]
    "Mosler Powered Luscombe Makes First Flight". Air Progress. March 1993.
Share this article:

This article uses material from the Wikipedia article Mosler_Red_82X, and is written by contributors. Text is available under a CC BY-SA 4.0 International License; additional terms may apply. Images, videos and audio are available under their respective licenses.