NASA NTRS · 20110014012
Project Morpheus Main Engine Development and Preliminary Flight Testing
Abstract
A LOX/Methane rocket engine was developed for a prototype terrestrial lander and then used to fly the lander at Johnson Space Center. The development path of this engine is outlined, including unique items such as variable acoustic damping and variable film cooling.
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Morehead, Robert L.. 2011-07-30. Project Morpheus Main Engine Development and Preliminary Flight Testing. https://ntrs.nasa.gov/citations/20110014012
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