Accession Number : ADD004540

Title :   Baffled Combustion Chamber.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE NAVY WASHINGTON D C

Personal Author(s) : Schadow,Klaus

Report Date : Oct 1977

Pagination or Media Count : 4

Abstract : An apparatus to improve combustion efficiency of solid fueled ramjets by reducing or slowing down the mixing between the air stream and the combustion zone near the fuel grain. The mixing process is altered by placing a control device parallel to the longitudinal axis of the combustion chamber and spaced from the interior wall of the solid fuel. The device may take the form of a co-axial tube which may be perforated slotted or segmented. (Author)

Descriptors :   *Patents, *Solid propellant rocket engines, *Ramjet engines, *Combustion chambers, Combustion stability, Baffles, Mixing, Air

Subject Categories : Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE