COOLED SOLID PROPELLANT ROCKET NOZZLES
Abstract
Contents: Uncooled nozzle tests Test data reduction - core gas convection coefficients Method of data reduction Predicted core gas convection coefficients Comparison of predicted and derived coefficients Labyrinth seal tests Determination of the core gas convection coefficients Methods of predicting core gas convection coefficients Determination of the core gas properties
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 30, 1962
- Accession Number
- AD0291559
Entities
People
- Philip Wacks