NASA NTRS · 20000109907
MC-1 Nozzle Testing Results
Abstract
This document is the presentation graphics which reviews the test results of the MC-1 Nozzle. The MC-1 Nozzle was originally designed for a low cost engine for an expendable booster. It was modified for use in the X-34 propulsion plant. With this design the nozzle and chamber are one piece. The presentation reviews the design goals, the materials and fabrication. The tests and results are reviewed in considerable detail. Included are pictures of the nozzle, and diagrams of the nozzle geometry
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Peters, Warren, Turner, James E.. 2000-01-01. MC-1 Nozzle Testing Results. https://ntrs.nasa.gov/citations/20000109907
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