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Injection Principles from Combustion Studies in a 200-Pound-Thrust Rocket Engine Using Liquid Oxygen and Heptane
Author:
Heidmann, M. F.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E55C22
Link:
https://digital.library.unt.edu/ark:/67531/metadc64210/
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