{
"item_title" : "The Design and Testing of a Miniature Turbofan Engine",
"item_author" : [" Nasa Technical Reports Server (Ntrs)", "Gary B. Cosentino", "James E. Murray "],
"item_description" : "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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"retail_price" : "15.75", "online_price" : "15.75", "our_price" : "15.75", "club_price" : "15.75", "savings_pct" : "0", "savings_amt" : "0.00", "club_savings_pct" : "0", "club_savings_amt" : "0.00", "discount_pct" : "10", "store_price" : ""
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The Design and Testing of a Miniature Turbofan Engine
Overview
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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Details
- ISBN-13: 9781289267353
- ISBN-10: 1289267359
- Publisher: Bibliogov
- Publish Date: July 2013
- Dimensions: 9.69 x 7.44 x 0.08 inches
- Shipping Weight: 0.2 pounds
- Page Count: 40
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