Investigations in chemical rocket propulsion Final report, 1 Jul. 1964 - 31 Dec. 1967
Heat and mass transfer characteristics of liquid film cooling, optimum thrust nozzle contours, liquid propellant combustion processes and ignition of solid propellants
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| Format: | Report |
| Sprache: | eng |
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| Zusammenfassung: | Heat and mass transfer characteristics of liquid film cooling, optimum thrust nozzle contours, liquid propellant combustion processes and ignition of solid propellants |
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