Refinery process studies have indicated that the relaxation of the JP-5 freeze point specification is a viable means of increasing jet fuel availability. The Naval Air Propulsion Center is investigating the impact of higher freeze point fuels on naval aircraft operations. Six fuels, with freeze points ranging from −55°F to +10°F, were tested in two instrumented external fuel tanks. Thirty hours of flight test and one hundred hours of wind tunnel test data have been accumulated. This information is being used in conjunction with laboratory and bench scale test data to support the development of a three dimensional computer code. This code will predict fuel cool down and hold-up (unpumpable frozen fuel) for any fuel tank geometry during a mission. Initial results indicate that the current JP-5 freeze point specification of −51°F is conservative and could be safely relaxed.
Skip Nav Destination
ASME 1986 International Gas Turbine Conference and Exhibit
June 8–12, 1986
Dusseldorf, West Germany
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-7930-6
PROCEEDINGS PAPER
Impact of Higher Freeze Point Fuels on Naval Aircraft Operations
R. A. Kamin,
R. A. Kamin
Naval Air Propulsion Center, Trenton, NJ
Search for other works by this author on:
P. M. McConnell
P. M. McConnell
Boeing Military Airplane Company, Seattle, WA
Search for other works by this author on:
R. A. Kamin
Naval Air Propulsion Center, Trenton, NJ
P. M. McConnell
Boeing Military Airplane Company, Seattle, WA
Paper No:
86-GT-262, V003T06A018; 6 pages
Published Online:
April 1, 2015
Citation
Kamin, RA, & McConnell, PM. "Impact of Higher Freeze Point Fuels on Naval Aircraft Operations." Proceedings of the ASME 1986 International Gas Turbine Conference and Exhibit. Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations. Dusseldorf, West Germany. June 8–12, 1986. V003T06A018. ASME. https://doi.org/10.1115/86-GT-262
Download citation file:
229
Views
Related Proceedings Papers
Related Articles
A Proposal for Integration of Wind Tunnel and Engine Test Programs for the Evaluation of Airframe-Propulsion Compatibility Using Numerical Simulations
J. Eng. Gas Turbines Power (July,2002)
Hydrazine Monopropellant Reciprocating Engine Development
J. Eng. Ind (November,1979)
Boundary Layer Ingestion Propulsion: A Review on Numerical Modeling
J. Eng. Gas Turbines Power (December,2020)
Related Chapters
Fuels, Fuel Piping and Fuel Storage
Handbook for Cogeneration and Combined Cycle Power Plants, Second Edition
Modeling of the Processes in the Airport Area (PSAM-0468)
Proceedings of the Eighth International Conference on Probabilistic Safety Assessment & Management (PSAM)
Scope
Consensus on Operating Practices for the Control of Feedwater and Boiler Water Chemistry in Modern Industrial Boilers (CRTD 34)