Works matching DE "ATMOSPHERIC braking of space vehicles"
Results: 11
Proposal for Creating a Device for Deorbiting Low-Earth-Orbit CubeSats.
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- Solar System Research, 2018, v. 52, n. 7, p. 606, doi. 10.1134/S003809461807016X
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Design Experience of a Demonstrator Descent Vehicle Introducing Aeroelastic Deployable Structural Elements to Space Engineering.
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- Solar System Research, 2018, v. 52, n. 7, p. 590, doi. 10.1134/S0038094618070031
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Transformable descent vehicles.
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- Solar System Research, 2016, v. 50, n. 7, p. 489, doi. 10.1134/S0038094616070200
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Design principles of descent vehicles with an inflatable braking device.
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- Solar System Research, 2013, v. 47, n. 7, p. 491, doi. 10.1134/S0038094613070022
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Venus Express lives.
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- Astronomy & Geophysics, 2014, v. 55, n. 1, p. 5.10, doi. 10.1093/astrogeo/atu208
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Analysis of the dynamics of the deployed aerodynamic space tether system.
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- Cosmic Research, 2017, v. 55, n. 5, p. 371, doi. 10.1134/S0010952517050057
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Advances in the linear/nonlinear control of aeroelastic structural systems.
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- Acta Mechanica, 2005, v. 178, n. 3-4, p. 147, doi. 10.1007/s00707-005-0222-6
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Solar Rotation Effects in Martian Thermospheric Density as Revealed by Five Years of MAVEN Observations.
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- Journal of Geophysical Research. Planets, 2022, v. 127, n. 1, p. 1, doi. 10.1029/2021JE007036
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The Wave Origins of Longitudinal Structures in ExoMars Trace Gas Orbiter (TGO) Aerobraking Densities.
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- Journal of Geophysical Research. Space Physics, 2021, v. 126, n. 2, p. 1, doi. 10.1029/2020JA028769
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Motion Modeling and Deployment Control of a Long Tethered Spacecraft System with an Atmospheric Sounder.
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- Engineering Letters, 2018, v. 26, n. 4, p. 478
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- Article
Spacecraft aerodynamics and trajectory simulation during aerobraking.
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- Applied Mathematics & Mechanics, 2010, v. 31, n. 9, p. 1063, doi. 10.1007/s10483-010-1342-x
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- Article