Accession Number : AD0419883
Title : IGNITION AND COMBUSTION OF SOLID PROPELLANTS.
Descriptive Note : Technical rept., 1 Oct 61-30 Sep 62,
Corporate Author : UTAH UNIV SALT LAKE CITY
Personal Author(s) : Mitchell,Rex C. ; Keller,John A.
Report Date : 30 SEP 1962
Pagination or Media Count : 35
Abstract : The response of several selected composite propellants subjected to surface heat fluxes was experimentally studied. The surface propellant samples were subjected to thermal-radiation heat fluxes from 1 to 13.5 cal/sec sq cm and convective heat fluxes from 30 to 100 cal/sec sq cm. Parallel theoretical studies, which were guided by the experimental results, have given a satisfactory explanation of the general character of the ignition process. The scope of this research work has been broadened to include several phases of the combustion of solid propellants. (Author)
Descriptors : (*SOLID ROCKET PROPELLANTS, IGNITION), (*IGNITION, SOLID ROCKET PROPELLANTS), COMBUSTION, THEORY, SURFACES, HEAT TRANSFER, THERMAL RADIATION
Distribution Statement : APPROVED FOR PUBLIC RELEASE