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High speed commercial transport fuels considerations and research needsNASA is currently evaluating the potential of incorporating High Speed Civil Transport (HSCT) aircraft in the commercial fleet in the beginning of the 21st century. NASA sponsored HSCT enabling studies currently underway with airframers and engine manufacturers, are addressing a broad range of technical, environmental, economic, and related issues. Supersonic cruise speeds for these aircraft were originally focused in the Mach 2 to 5 range. At these flight speeds, both jet fuels and liquid methane were considered potential fuel candidates. For the year 2000 to 2010, cruise Mach numbers of 2 to 3+ are projected for aircraft fuel with thermally stable liquid jet fuels. For 2015 and beyond, liquid methane fueled aircraft cruising at Mach numbers of 4+ may be viable candidates. Operation at supersonic speeds will be much more severe than those encountered at subsonic flight. One of the most critical problems is the potential deterioration of the fuel due to the high temperature environment. HSCT fuels will not only be required to provide the energy necessary for flight, but will also be subject to aerodynamic heating and, will be required to serve as the primary heat sink for cooling the engine and airframe. To define fuel problems for high speed flight, a fuels workshop was conducted at NASA Lewis Research Center. The purpose of the workshop was to gather experts on aviation fuels, airframe fuel systems, airport infrastructure, and combustion systems to discuss high speed fuel alternatives, fuel supply scenarios, increased thermal stability approaches and measurements, safety considerations, and to provide directional guidance for future R and D efforts. Subsequent follow-up studies defined airport infrastructure impacts of high speed fuel candidates. The results of these activities are summarized. In addition, an initial case study using modified in-house refinery simulation model Gordian code (1) is briefly discussed. This code can be used to simulate different types of refineries, emphasizing jet fuel production and relative cost factors.
Document ID
19900012553
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lee, C. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Niedzwiecki, R. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Subject Category
Propellants And Fuels
Report/Patent Number
NAS 1.15:102535
E-5345
NASA-TM-102535
Report Number: NAS 1.15:102535
Report Number: E-5345
Report Number: NASA-TM-102535
Meeting Information
Meeting: Symposium on the Structure of Future Jet Fuels 2
Location: Miami Beach, FL
Country: United States
Start Date: September 10, 1989
End Date: September 15, 1989
Sponsors: American Chemical Society
Accession Number
90N21869
Funding Number(s)
PROJECT: RTOP 535-05-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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