Accession Number:

ADD005615

Title:

Low Viscosity-High Flash Point Ramjet and Turbojet Fuels.

Descriptive Note:

Patent,

Corporate Author:

DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s):

Report Date:

1977-06-07

Pagination or Media Count:

2.0

Abstract:

A method for propelling a ramjet or turbojet engine wherein a fuel consisting essentially of a mixture of a fraction of petroleum distillate having a boiling point of from 380 F to 415 F and butylbenzene is used. Author

Subject Categories:

  • Combustion and Ignition
  • Fuels

Distribution Statement:

APPROVED FOR PUBLIC RELEASE