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Antimisting kerosene: Base fuel effects, blending and quality control techniquesThe problems associated with blending of the AMK additive with Jet A, and the base fuel effects on AMK properties are addressed. The results from the evaluation of some of the quality control techniques for AMK are presented. The principal conclusions of this investigation are: significant compositional differences for base fuel (Jet A) within the ASTM specification DI655; higher aromatic content of the base fuel was found to be beneficial for the polymer dissolution at ambient (20 C) temperature; using static mixer technology, the antimisting additive (FM-9) is in-line blended with Jet A, producing AMK which has adequate fire-protection properties 15 to 20 minutes after blending; degradability of freshly blended and equilibrated AMK indicated that maximum degradability is reached after adequate fire protection is obtained; the results of AMK degradability as measured by filter ratio, confirmed previous RAE data that power requirements to decade freshly blended AMK are significantly higher than equilibrated AMK; blending of the additive by using FM-9 concentrate in Jet A produces equilibrated AMK almost instantly; nephelometry offers a simple continuous monitoring capability and is used as a real time quality control device for AMK; and trajectory (jet thurst) and pressure drop tests are useful laboratory techniques for evaluating AMK quality.
Document ID
19840008283
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Yavrouian, A. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ernest, J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sarohia, V.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1984
Publication Information
Publisher: FAA
Subject Category
Propellants And Fuels
Report/Patent Number
NASA-CR-174509
AD-A137852
NAS 1.26:174509
JPL-PUB-83-96
DOT/FAA/CT-83/36
Report Number: NASA-CR-174509
Report Number: AD-A137852
Report Number: NAS 1.26:174509
Report Number: JPL-PUB-83-96
Report Number: DOT/FAA/CT-83/36
Accession Number
84N16351
Funding Number(s)
CONTRACT_GRANT: DTFA03-80-A-00215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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