Accession Number:

AD0602806

Title:

COOLED SOLID PROPELLANT ROCKET NOZZLES,

Descriptive Note:

Final rept., vol. 2,

Corporate Author:

ARDE-PORTLAND INC PARAMUS N J

Personal Author(s):

Report Date:

1964-06-15

Pagination or Media Count:

195.0

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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE