12.1.2017 Static Performance Prediction of Hot-Gas Flapper-Nozzle Actuator

2017 (1); 78-83 Language: Russian Annotation: The basic mathematical relations are considered to construct static characteristics of nozzle-shutter twostage piston pneumatic drive [...]

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16.1.2020 Parameters of the supersonic jet of a block propulsion system, flowing into a gas duct, considering chemical kinetics of gas-cycle transformations

The presented work contains simulation of liquid rocket engine combustion products jet flowing into the gas duct at the rocket lift-off, taking into account the [...]

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10.1.2020 Calculation and selection of parameters for a propellant consumption diagram of dual-thrust main SRM

The presented method allows quickly determining the conditions needed to fulfill required propellant combustion products consumption diagrams and in case of [...]

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10.1.2018 The Rocket Propellant Vapors and Water Solutions Neutralization Units. The Accumulated Experience and Prospects of Updating the Neutralization Units

Thermodynamic and Thermophysical Properties of Combustion Products.

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8.2.2017 Analysis Method of Nitrogen Tetroxide Tanks Generating Pressurization Systems

Thermal Dynamic and Thermal Physical properties of Combustion Products.

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11.1.2017 Environmental Safety of Bench Testing the Advanced Solid-Propellant Rocket Motors

2017 (1); 70-77 Language: Russian Annotation: The mathematical models are presented and the calculations are made of lower atmosphere contamination with solid propellant [...]

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9.1.2016 Evaluation of SRM Intraballistic Parameters Scatter by Monte-Carlo Method

2016 (1); 59-62 Language: Russian Annotation: The purpose of work is development of simple and accurate procedure of calculation of scatter of SRM intraballistic parameters – [...]

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