Studies carried out by U S Air Force Aero Propulsion Laboratory on effects of subsonic flight environment on fuels refined for high Mach number application; high temperature fuel property requirements and hydrocarbon composition to meet these requirements; fuel compositions and low temperatures; results of wing tank pumpability tests; materials compatibility of high temperature fuels; it is concluded that establishment of specification criteria to obtain high temperature fuel suitable for subsonic and supersonic use will adversely affect cost and availability of product.
High temperature hydrocarbon fuels and subsonic flight environments
SAE -- Paper
SAE Meeting ; 1965
1965
10 pages
Conference paper
English
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High Temperature Hydrocarbon Fuels and Subsonic Flight Environments
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