Boeing T50-BO-8A (502-10VC) Turboshaft Engine

Object Details

Physical Description: Type: Turboshaft; Power Rating: 224 kW (300 hp) at 28,380 rpm; Compressor: Single-stage centrifugal; Combustor: 2 combustion chambers; Turbine: Single-stage axial; Weight: 152 kg (334 lb)
Summary: In the mid-1940s, Boeing engineers conducted research to become familiar with gas turbines, but it became apparent that the research engines were significant in themselves. First engine run was the 667 N (150 lb) thrust Model 500 turbojet, closely followed by the 119 kw (160 shp) Model 502 turboprop. Because no applications materialized for the turbojet, efforts were focused on the Model 502, initially developed as a turboprop and later as the more widely used turboshaft engine, first delivered in 1949.; In late-1951, a Model 502 powered Kaman K-225 helicopter became the world's first gas turbine-powered helicopter, and, in late-1952, a Model 502 powered Cessna XL-19B Bird Dog became the world's first turboprop-powered light aircraft.; By the mid-1960s, significant power and reliability improvements produced the Model 502-10VC, the first U.S. turbine engine in the 149 to 224 kw (200 to 300 shp) range to receive an approved 150-hour qualification. This artifact powered the Gyrodyne QH-50C (DSN-3) drone helicopter.

Credit Line: Transferred from the U.S. Navy, Naval Supply Center, Norfolk, Virginia

Circa 1950s

Materials: Aluminum, Steel, Paint, Rubber, Copper, Stainless Steel, Titanium
Dimensions: Length 101.6 cm (40.0 in.), Diameter 61.0 cm (24.0 in.)

National Air and Space Museum

GUID (Link to Original Record): http://n2t.net/ark:/65665/nv9bbcc2de6-ead1-4db5-8653-41ed6ed795ab