THEORY OF SOLID FUEL ROCKET ENGINES
Abstract
This is a basic text on rocket fuels intended for specialists and engineers. Basic data is drawn from U. S. rocket technology. Covered in the text are: (1) basic fundamentals of rocket fuels, composition, caloricity; (2) progressive burn characteristics; (3) gas flow equations, pressure characteristics; (4) engine tuning; (5) heat shielding; and (6) thrust chamber and atmospheric dependences.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 26, 1968
- Accession Number
- AD0684023
Entities
People
- G. Yu. Mazing
- N. E. Prudnikov
- Ya. M. Shapiro