DIGITAL MODERNIZATION OF A TEST STAND FOR THERMAL AND THRUST TESTING OF LIQUID ROCKET ENGINES
DOI:
https://doi.org/10.30890/2567-5273.2025-42-01-006Keywords:
Liquid rocket engine, Test stands, Propellant type (O₂/CH₄), Digital modernizationAbstract
This article presents the results of the digital modernization of a test stand for thermal and thrust testing of a low-thrust liquid rocket engine using gaseous O₂/CH₄ propellants. The aim of the article is to introduce the metrologically correct system,References
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