Accession Number : ADD004218

Title :   Split Flow Injector for Solid Fuel Ramjets.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s) : Humphrey,John M ; Holzmn,Allen L

Report Date : 28 Jun 1977

Pagination or Media Count : 5

Abstract : A split flow injector for solid fuel ramjets (SDRJ) having a tube injected into the injector port of a SFRJ to split the air into two streams wherein the primary airflow through the annular area around the tube is injected into the recirculation region just inside the injector port to stabilize combustion. (Author)

Descriptors :   *Patents, *Injectors, *Solid jet engine fuels, *Ramjet engines, Splitting, Air flow, Combustion stability, Annular nozzles, Weight, Volume, Pressure, Recirculation, Flow fields

Subject Categories : Fuels
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE