The Turbomeca Palouste is a French gas turbine engine, first run in 1952.[1] Designed purely as a compressed air generator, the Palouste was mainly used as a ground-based aircraft engine starter unit. Other uses included rotor tip propulsion for helicopters.
^Gunston 1989, p.170.
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consumption: 57 kg (125 lb) per hour at maximum power Comparable engines TurbomecaPalouste Related lists List of aircraft engines Wikimedia Commons has media...
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