The Design and Testing of a Miniature Turbofan Engine - Paperback
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by Nasa Technical Reports Server (Ntrs) (Created by), Gary B. Cosentino (Author), James E. Murray (Author)
Off-the-shelf jet propulsion in the 50 - 500 lb thrust class sparse. A true twin-spool turbofan in this range does not exist. Adapting an off-the-shelf turboshaft engine is feasible. However the approx.10 Hp SPT5 can t quite make 50 lbs. of thrust. Packaging and integration is challenging, especially the exhaust. Building on our engine using a 25 Hp turboshaft seems promising if the engine becomes available. Test techniques used, though low cost, adequate for the purpose.
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