COOLED SOLID PROPELLANT ROCKET NOZZLES,
Abstract
A study was made to evaluate the potential of the liquid metal lithium as a coolant for solid propellant rocket nozzles. The program plan included the analysis, design, and testing of two cooling systems: Convection; and Spray film. A literature survey was made to review the state-of-the-art of rocket nozzle cooling. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 15, 1964
- Accession Number
- AD0602805
Entities
People
- Sidney Elkind