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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