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ARP949B - Turbine Engine Starting System Design Requirements

Details
Document Number: ARP949B
Revision Number: B
Title
Turbine Engine Starting System Design Requirements
Scope
This SAE Aerospace Recommended Practice (ARP) defines and establishes a standard presentation of data for gas turbine propulsion engine starter characteristics in graphs and curves. The data presentation applies to both pneumatic and hydraulic energy source starting systems.<p>This recommended practice is intended to define and establish, where applicable, a standard presentation of the engine characteristics required for the determination of a satisfactory starting system for aircraft gas turbine engines.
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