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RP-1 and JP-8 Thermal Stability ExperimentsThis work experimentally investigates the effect of fuel composition changes on jet and rocket fuel thermal stability. A High Reynolds Number Thermal Stability test device evaluated JP-8 and RP-1 fuels. The experiment consisted of an electrically heated, stainless steel capillary tube with a controlled fuel outlet temperature. An optical pyrometer monitored the increasing external temperature profiles of the capillary tube as deposits build inside during each test. Multiple runs of each fuel composition provided results on measurement repeatability. Testing a t two different facilities provided data on measurement reproducibility. The technique is able to distinguish between thermally stable and unstable compositions of JP-8 and intermediate blends made by combining each composition. The technique is also able to distinguish among standard RP-1 rocket fuels and those having reduced sulfur levels. Carbon burn off analysis of residue in the capillary tubes on the RP-1 fuels correlates with the external temperature results.
Document ID
20050204031
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Brown, Sarah P.
(Alabama Univ. Huntsville, AL, United States)
Emens, Jessica M.
(Alabama Univ. Huntsville, AL, United States)
Frederick, Robert A., Jr.
(Alabama Univ. Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
July 15, 2005
Subject Category
Propellants And Fuels
Report/Patent Number
AlAA Paper 2005-3850
Report Number: AlAA Paper 2005-3850
Meeting Information
Meeting: AIAA 41st Joint Propulsion Conference and Exhibit
Location: Tucson, AZ
Country: United States
Start Date: July 10, 2005
End Date: July 14, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NCC8-200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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