Found: 11
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On the Use of Inflatable Decelerators in the Design of Spacecraft Intended for the Study of Venus.
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- Solar System Research, 2020, v. 54, n. 7, p. 595, doi. 10.1134/S0038094620070059
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- Article
On the Dynamics of Atmospheric Gas Filling the Interior of a Prospective Descent Module During Descent in the Atmosphere of Mars.
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- Solar System Research, 2020, v. 54, n. 7, p. 574, doi. 10.1134/S0038094620070060
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- Article
Numerical Study of Physical and Chemical Processes in the Shock Layer on the Trajectory of a Return Vehicle in the Atmosphere.
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- Solar System Research, 2019, v. 53, n. 7, p. 606, doi. 10.1134/S0038094619070104
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Study of Aerodynamics of a Prospective Descent Module Descending in the Atmosphere of Mars.
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- Solar System Research, 2019, v. 53, n. 7, p. 500, doi. 10.1134/S0038094619070098
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- Article
Software Package for the Development of Thermal Protection Systems for Spacecraft Descent into the Atmospheres of Planets.
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- Solar System Research, 2018, v. 52, n. 7, p. 578, doi. 10.1134/S0038094618070109
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- Article
How Particles in the Martian Atmosphere Influence the Thermal Protection Structure of the Descent Module EXOMARS-2.
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- Solar System Research, 2017, v. 51, n. 7, p. 628, doi. 10.1134/S003809461707005X
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Computational and theoretical investigation of Mars's atmospheric impact on the descent module 'Exomars-2018' under aerodynamic deceleration.
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- Solar System Research, 2016, v. 50, n. 7, p. 498, doi. 10.1134/S0038094616070054
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- Article
Aerodynamic design of a descent vehicle in the Martian atmosphere under the exomars project.
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- Solar System Research, 2014, v. 48, n. 7, p. 541, doi. 10.1134/S0038094614070089
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- Article
On the boundary conditions on a shock wave for hypersonic flow around a descent vehicle.
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- Solar System Research, 2013, v. 47, n. 7, p. 520, doi. 10.1134/S003809461307006X
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- Article
Program package for the computer-aided aerodynamic design system for descent vehicles in planetary atmospheres.
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- Solar System Research, 2012, v. 46, n. 7, p. 542, doi. 10.1134/S003809461207012X
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- Article
Calculation of Radiation Heat Transfer in Problems of Flow past Bodies with Account for Heat-Shield Coating Mass Loss.
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- Fluid Dynamics, 2004, v. 39, n. 4, p. 633, doi. 10.1023/B:FLUI.0000045679.30291.9e
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- Article