SYSTEM AND METHODS FOR MANUFACTURING REGENERATIVELY COOLED ROCKET THRUST CHAMBER NOZZLES
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United States of America Patent
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Sep 5, 2019
app pub date -
Mar 1, 2019
filing date -
Mar 1, 2018
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Abstract
In the area of rocket engines, regeneratively cooled rocket engines currently undergo long manufacturing time frames. This deters the speed of the development process resulting in a longer time to get to the market with a proven new design. There is a need to create methods that can manufacture regeneratively cooled rocket engines faster with a quick time to the market. This disclosure relates to faster methods for manufacturing regeneratively cooled rocket thrust chamber nozzles that use rocket propellant fluids to cool the chamber walls of the nozzle itself before being injected and burned. Furthermore, the new methods lead to enhanced designs that could enable reusable rocket engines by limiting overall fatigue with novel materials.
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