Nonstationary Combustion of Solid Rocket Fuels,
Abstract
In recent years the study of nonstationary combustion has been intensely conducted in many countries. This is conditioned by the fact that almost all processes of combustion which occur in rocket engines (ignition, transient conditions of combustion, vibration combustion, extinction, etc.) are related to nonstationary combustion. In the report the theory of the nonstationary combustion of solid rocket propellants is discussed, and experimental data which refer to such combustion behavior are given. From a single viewpoint the majority of the phenomena which occur during the nonstationary combustion of solid rocket propellants is described.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 27, 1973
- Accession Number
- AD0767945
Entities
People
- B. V. Novozhilov
Organizations
- National Air and Space Intelligence Center