Accession Number : AD0829016
Title : RESEARCH ON CONTROL OF ROCKET EXHAUST RADIATION, REPORT OF PRELIMINARY DATA. MODEL 7,
Corporate Author : GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV
Personal Author(s) : Leo, P. P.
Report Date : 27 JAN 1958
Pagination or Media Count : 8
Abstract : The objective was to determine: (a) if rocket exhaust radiation can be reduced by means of fuel additives and (b) the radiation from pure hydrocarbons that are typical fuel components. (Author)
Descriptors : (*LIQUID PROPELLANT ROCKET ENGINES, THERMAL RADIATION), (*EXHAUST GASES, THERMAL RADIATION), FUEL ADDITIVES, LIQUID ROCKET FUELS, HYDROCARBONS, COMBUSTION, EXPERIMENTAL DATA, EXHAUST NOZZLES, HEAT TRANSFER, STATISTICAL ANALYSIS.
Subject Categories : Thermodynamics
Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE