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