Low Viscosity Air Breathing Missile Fuel.
Abstract
An improved ramjet fuel consisting of hydrogenated hydrocarbons uses a minimum weight percentage of 50% tetrahydromethylcyclopentadiene dimer (TH-dimer) with about 50% by wt. exo-tetrahydrodicyclopentadiene (Exo-THDC). The mixture exceeds U.S. Navy flash point requirements of 60 C while yielding a lower viscosity than TH-dimer alone. Volumetric heating properties of the mixture make it an excellent ramjet fuel. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 29, 1982
- Accession Number
- ADD009515
Entities
People
- George W. Burdette
- Lewis Hall
Organizations
- United States Department of the Navy