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SBIR/STTR

Low Erosion Ceramic Composite Liners for Improved Performance of Ablative Rocket Thrust Chambers, Phase II

Completed Technology Project

Project Introduction

Low Erosion Ceramic Composite Liners for Improved Performance of Ablative Rocket Thrust Chambers, Phase II
Advanced liquid rocket propulsion systems must achieve longer burn times without performance degradation to allow the lowest cost per kilogram access to space. Ablative thrust chambers have an extensive heritage and are the low cost approach to fabricating rocket thrust chambers. More »

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This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.

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