Barrier Ring Injector.
Abstract
The patent application relates to a rocket engine injector device including three flanged concentric annular members and a manifold ring assembled to provide the high injection density required for barrier cooling. The barrier ring assembly includes an inner oxidizer metering ring serving as an oxidizer feed and a second ring for feeding oxidizer and metering fuel positioned around the inner ring. A third ring is fitted over the second ring for feeding fuel thereto. A fourth ring positioned around the third ring serves as a propellant manifold for barrier cooling the injector assembly.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 29, 1972
- Accession Number
- AD0164558
Entities
People
- Kin Y. Wong
Organizations
- United States Department of the Air Force