Abstract
The paper deals with the case of fuel deposition in the oxidizer tank of the space stage of the rocket using two low-thrust engines before re-starting the main engine. In addition, confirmed a computational-experimental method for determining the required time for fuel deposition, which combines experimental testing and numerical simulation of fuel deposition, which allows carrying out the necessary research with the required accuracy and significantly reducing the amount of testing and the need for material and technical equipment of the experimental base.
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