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)
Cooled Solid Propellant Rocket Nozzles
1964
2 pages
Report
No indication
English
Cooled Solid Propellant Rocket Nozzles
NTIS | 1964
|Fabrication of tungsten for solid-propellant rocket nozzles
Engineering Index Backfile | 1961
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