50-4 HO-10-600 INJECTOR – FUEL LIQUID HYDROGEN OXIDANT – LIQUID OXYGEN CHAMBER PRESSURE 600 PSI POUNDS PER SQUARE INCH 5000 POUND THRUST
A liquid hydrogen-liquid oxygen propellant injector designed at the NACA Lewis laboratory (1956).
Image Credit: NASA/BILL BOWLES
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https://www.nasa.gov/image-detail/grc-1956-c-42285/
Image CreditNASA/BILL BOWLES
Size2288x2314px