page_title: Turbomeca Palouste
section_title: Specifications (Palouste 4)
hierarchical_section_title: Turbomeca Palouste / Specifications (Palouste 4)
context_page_description: The Turbomeca Palouste is a French gas turbine engine, first run in 1952. 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.
context_section_description: Data from Flight :BRITISH POWER UNITS 1953,
caption: Palouste engine fitted to a Sud-Ouest Djinn helicopter
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