Turboméca Bastan
From Wikipedia, the free encyclopedia
The Turboméca Bastan was a turboprop engine developed in France in 1957. Early models developed 650 shp (485 kW), but by 1965 this had been increased to 1,048 shp (780 kW) with the Bastan VII.
The engine's principal application was the Aérospatiale N 262 airliner.
[edit] References
- Gunston, Bill (1986). World Encyclopedia of Aero Engines. Wellingborough: Patrick Stephens, 164.
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