{
"item_title" : "The General Aviation Propulsion (Gap) Program",
"item_author" : [" Philip Poinsatte", "Nasa Technical Reports Server (Ntrs)", "Et Al "],
"item_description" : "The General Aviation Propulsion (GAP) Program Turbine Engine Element focused on the development of an advanced small turbofan engine. Goals were good fuel consumption and thrust-to-weight ratio, and very low production cost. The resulting FJX-2 turbofan engine showed the potential to meet all of these goals. The development of the engine was carried through to proof of concept testing of a complete engine system. The proof of concept engine was ground tested at sea level and in altitude test chambers. A turboprop derivative was also sea-level tested.",
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The General Aviation Propulsion (Gap) Program
Overview
The General Aviation Propulsion (GAP) Program Turbine Engine Element focused on the development of an advanced small turbofan engine. Goals were good fuel consumption and thrust-to-weight ratio, and very low production cost. The resulting FJX-2 turbofan engine showed the potential to meet all of these goals. The development of the engine was carried through to proof of concept testing of a complete engine system. The proof of concept engine was ground tested at sea level and in altitude test chambers. A turboprop derivative was also sea-level tested.
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Details
- ISBN-13: 9781287230205
- ISBN-10: 1287230202
- Publisher: Bibliogov
- Publish Date: July 2013
- Dimensions: 9.69 x 7.44 x 0.14 inches
- Shipping Weight: 0.31 pounds
- Page Count: 68
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