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Turbojet UAV Fuel Metering Pump Case Study by chandu306 is a document available to read on EtoBox.

The document describes a family of turbojet engines rated from 30 to 100 lbf of thrust designed for expendable military UAV applications. The engines use components from turbochargers for turbines, compressors, and combustors. The fuel system features an electronically controlled fuel pump from Cascon that provides precise fuel flow for engine operation and cooling.

Author
chandu306
Language
EN