SELF-COOLED ROCKET NOZZLES.
Abstract
The work performed during the second quarter of the second year of a program to advance the self-cooled rocket nozzle concept is reported. Modifications to the computer-programmed theoretical analysis of self-cooling are described. A major addition to the analysis is the calculation of cases for composites of the heterogeneous matrix porosity which indicate the manner by which the self-cooling concept may be optimized. Fabrication procedures for the production of composites of complex matrix microstructure are described. The current status and future of the program are discussed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 27, 1964
- Accession Number
- AD0439421
Entities
People
- J. D. Seader
- P. Schwarzkopf
Organizations
- Rocketdyne