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Effect of combustion-chamber pressure and nozzle expansion ratio on theoretical performance of several rocket propellant systems
Author:
Morrell, Virginia E
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E50C30
Link:
https://digital.library.unt.edu/ark:/67531/metadc58415/
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