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