A Highly Compounded Two-Cycle Radial Light-Plane Engine Advance Development Div., McCulloch Corporation

Format:

Conference/Event

Author/Creator:

Dooley, J. L., author.

Conference Name:

National Aeronautic Meeting and Production Forum (1966-04-25 : New York, New York, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1966

Summary:

The authors review the requirements, describe some of the unusual design features and characteristics, and present the performance and weight data for the new McCulloch TSIR-5190 aircraft engine. This powerplant is a highly turbosupercharged, two-stroke cycle, direct fuel injection, liquid cooled, 5 cyl radial engine of 190 cu inches displacement.Maximum rated horsepower is 270 at 3600 rpm, and the brake specific fuel consumption, over the range from half-to full power, is below 0.5 lb/bhp-hours The estimated "ready to fly" weight for the production engine is 365 lb. Some comparisons are made with currently available engines

Notes:

Vendor supplied data

Publisher Number:

660173

Access Restriction:

Restricted for use by site license