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Installation of a 28,000-pound thrust gaseous hydrogen-FLOX engine at J-1 during November 1966 study heat transfer at the nozzle.
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Installation of a 28,000-pound thrust gaseous hydrogen-FLOX engine at J-1 during November 1966 study heat transfer at the nozzle.
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- https://www1.grc.nasa.gov/historic-facilities/rockets-systems-area/j-site-rockets-system-test-site/
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