KINETIC STUDY OF ROCKET EXHAUST GASES.
Abstract
The initial objective of this program was to investigate the feasibility of devices for extraction of electrical energy from rocket engine exhaust streams. An extensive literature search was conducted, a comprehensive bibliography prepared (published in PB-153 966) and an analytic study performed based on a physical model deduced from the most accurate experimental evidence available. Subsequently, a study of the subtle changes induced in the solid propellant combustion process by introduction of additives was undertaken. These additives, in general, modify the burning rates of propellant material. Various optical diagnostic techniques were employed to identify species concentration by flame zones and to obtain localized temperatures and total visible radiation values with good time resolution. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 30, 1965
- Accession Number
- AD0615124