Liquid hydrocarbon air breather fuel

• US 4,410,749 A
• Filed: 10/13/1981
• Issued: 10/18/1983
• Est. Priority Date: 10/13/1981
• Status: Expired due to Fees

• Current Assignee: the united states of america as represented by the secretary of the navy
• Original Assignee: the united states of america as represented by the secretary of the navy
• Inventors: Burdette, George W.
• Primary Examiner(s): Warren, Charles F.
• Assistant Examiner(s): Harris-Smith Y.
• Application Number:
  US06/310,553
• Time in Patent Office: 735 Days
• Field of Search: 585/14, 585/21, 585/22, 585/23, 208/15
• US Class Current: 585/14
• CPC Class Codes: C10L 1/04 essentially based on blends of hydrocarbons

Abstract

A high energy, high density synthetic liquid hydrocarbon fuel, RJ-6, is pared by blending 60 weight percent perhydrodinorbornadiene, a synthetic fuel known as RJ-5, and 40 weight percent exo-tetrahydrocyclopentadiene, a synthetic fuel known as JP-10. This fuel is particularly suitable for use in air launched ramjet engine applications such as aircraft missile systems. This new fuel substantially meets the desirable viscosity, energy content, and flash point of the previously employed synthetic fuel blend while exhibiting superior storage characteristics in elastomeric fuel systems used in missile applications.

Claims

1. A composition of matter having a density of about 1.020 gram/per cubic centimeter and a viscosity of about 8 centipoises at 20°

C., a viscosity of about 154 centipoises at -40°

C. and a flash point of about 66°

C., useful as a fuel, consisting essentially of about 60 weight percent RJ-5, a production run fuel having as components at least two different isomers of perhydrodinorbornadiene, and about 40 weight percent JP-10, exo-tetrahydrodicyclopentadiene.