650115: High Temperature Hydrocarbon Fuels and Subsonic Flight Environments - Technical Paper

Event: 1965 International Automotive Engineering Congress and Exposition

Authors

U. S. Air Force Aero Propulsion Laboratory

Abstract

Content: Studies on the effects of a subsonic flight environment on fuels refined for high Mach number application are reported. Requirements and hydrocarbon composition for fuel to withstand high Mach number stresses are cited and their compatibility with conventional systems at low temperatures is discussed.

Meta Tags

Topics: Hydrocarbons

Affiliated or Co-Author: U. S. Air Force Aero Propulsion Laboratory

Details

DOI: https://doi.org/10.4271/650115

Pages: 10

Citation: Hager, J., "High Temperature Hydrocarbon Fuels and Subsonic Flight Environments," SAE Technical Paper 650115, 1965, https://doi.org/10.4271/650115.

Additional Details

Publisher: SAE International

Published: Feb 1, 1965

Product Code: 650115

Content Type: Technical Paper

Language: English