NASA NTRS · 19750024092
Space shuttle orbit maneuvering engine
Abstract
Data on the performance, stability, and thermal characteristics of an OME operating with an alternate injector configuration and with alternate propellants was obtained. The design, manufacturing, and operating characteristics of an electroformed, regeneratively cooled thrust chamber were also derived. Subscale and full scale tests provide data relating to off-design and transient operation.
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Pauckert, R. P.. 1975-08-29. Space shuttle orbit maneuvering engine. https://ntrs.nasa.gov/citations/19750024092
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