Accession Number : ADD003400
Title : Burning Rate Modifiers for Solid Propellants.
Descriptive Note : Patent,
Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON D C
Personal Author(s) : Roberto,Francisco Q ; Crelier,Arnold M ; Lium,Gary D
Report Date : 28 Dec 1976
Pagination or Media Count : 3
Abstract : The patent relates to a solid propellant formulation which uses the addition of low levels of transition metal fluorides, such as cupric fluoride and ferric fluoride, as a modifying agent to increase the propellant burning rate while simultaneously decreasing its pressure exponent.
Descriptors : *Patents, *Solid rocket propellants, *Fluorides, *Metal compounds, Formulations, Burning rate, Fluorine compounds
Subject Categories : Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE