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SBIR/STTR

Propulsion Test Support Analysis with GPU Computing, Phase I

Completed Technology Project

Project Introduction

Propulsion Test Support Analysis with GPU Computing, Phase I
The design, development and staging of tests to certify liquid rocket engines usually require high-fidelity structural, fluid and thermal support analysis. These analyses are crucial to a successful engine test program since pressurization requirements, heat loads, cooling requirements and structural stresses are evaluated. More »

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