COMBUSTION AND PERFORMANCE STUDIES OF INJECTION PROCESSES IN A 200 POUND THRUST ROCKET ENGINE LIQUID OXYGEN LOX HEPTANE SYSTEM
Firing of a 200-pound thrust heptane and liquid oxygen rocket in Cell 13 of the Rocket Lab (1955).
Image Credit: NASA
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https://www.nasa.gov/image-detail/grc-1955-c-38038/
Image CreditNASA
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