COMBUSTION IRREGULARITIES IN SOLID PROPELLANTS.
Abstract
In studies employing the side-vented end-burner, the participation of the solid phase in acoustic oscillations was quantitatively confirmed and described. In cooperation with other laboratories, the usefulness of the burner for propellant evaluation was demonstrated. Initial experiments in a study of non-acoustic instability were performed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 04, 1966
- Accession Number
- AD0630409
Entities
People
- Norman W. Ryan
Organizations
- University of Utah