General Electric T58-GE-8F Turboshaft Engine
Object Details
- Manufacturer
- General Electric Aircraft Engines
- Physical Description
- Type: Turboshaft
- Power rating: 1,007 kW (1,350 shp) at 19,500 rpm
- Compressor: 10-stage axial
- Combustor: Annular
- Turbine: 2-stage axial for gas generator, single-stage axial free power turbine
- Weight: 138 kg (305 lb)
- Summary
- Developed under a 1953 U.S. Navy contract, the T58 was GE's first small gas turbine aircraft engine. Its first flight took place in 1957 in a modified Sikorsky HSS-1F helicopter powered by two YT58 engines. More than 6,000 T58 and CT58 (civilian version) engines were built between 1956 and 1984, most for military helicopters. A first-generation turbine engine, the T58 improved helicopter speed, payload, and safety.
- Among military helicopter applications were the Sikorsky SH-3 Sea King, Sikorsky HH-3E Jolly Green Giant, Kaman SH-2 Seasprite, Sikorsky HH-52 Sea Guard, and Boeing Vertol CH-46A Sea Knight. The CT58 was the first gas turbine helicopter engine certificated by the FAA, powering the Sikorsky S-62 for Los Angeles Airways beginning in late-1960. Other CT58-powered helicopters included the Sikorsky S-61 and Vertol 107.
- This artifact powered a Navy Sikorsky SH-3G utility helicopter. The -8F also powered the Marine Sikorsky VH-3A VIP helicopters for Presidential use, and similar HH-3A search and rescue helicopters.
- Credit Line
- Transferred from the U.S. Navy
- Circa 1960-68
- Inventory Number
- A19920060000
- Restrictions & Rights
- Usage conditions apply
- Type
- PROPULSION-Turbines (Jet)
- Dimensions
- Length 149 cm (58.6 in.), Width 52.6 cm (20.7 in.), Height 54.6 cm (21.5 in.)
- Country of Origin
- United States of America
- See more items in
- National Air and Space Museum Collection
- National Air and Space Museum
- Record ID
- nasm_A19920060000
- Metadata Usage (text)
- Not determined
- GUID (Link to Original Record)
- http://n2t.net/ark:/65665/nv9cb1548da-f646-4e17-b1e1-27b7798236fd