NASA NTRS · 20000112951
A Regeneratively-Cooled Thrust Chamber for the Fastrac Engine
Abstract
This document consists of presentation slides about the development of the regeneratively cooled thrust chamber for the Fastrac engine. The Fastrac engine was originally developed to demonstrate low cost design and fabrication methods. It was intended to be used in an expendable booster. The regen thrust chamber enables a more cost efficient test program. Using the low cost design and fabrication methodology designed for the 12K regeneratively cooled chamber, the contractor designed, developed and fabricated a regeneratively cooled thrust chamber for the Fastrac engine.
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Brown, Kendall, Sparks, Dave, Woodcock, Gordon, Jim Turner. 2000-01-01. A Regeneratively-Cooled Thrust Chamber for the Fastrac Engine. https://ntrs.nasa.gov/citations/20000112951
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