Abstract
The main objective of this work was to analyze main methods of measuring the thrust of rocket engines. It considers numerical and experimental (direct and indirect) method groups and an intermediate metjod group - computational and experimental, which combine the methods of both of the above categories.The work provides disadvantages and advantages of the indicated methods of registration of the differential thrust of rocket engines and considere its relevance. Solving the problem of estimating thrust asymmetry will make it possible to make changes and corrections in the operation of the rocket engine in advance.
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