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Title
Authors
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
Constructive actions for decreasing the acoustic pressure inside space-rocket products
Popov P.A., Sindyukov A.A.
Determining flow regimes around rocket boosters on a part of the launch orbit
Kharitonova A.N.
Analysis of the influence of the scheme of flight of the stage with a reactive recovry system on the energy characteristics of a two-stage medium class launch vehicle
Kuznetsov U.L., Ukraintsev D.S.
Promising technologies for solving boundary problems regarding the delivery of separating parts of carrier rockets with terminal targeting
Benevolsky S.V., Goncharenko V.I.
The process of ice formation on the surface of cryogenic tanks
Biryuk V.V., Shepelev A.I.
Determination of loads on perforated tank partition
Filipov A.G., Glazkov I.E.
Study of characteristics of the launch vehicle fuel line gas damper
Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.
Determination of mass-power propertions for parametric range of launch vehicle modifications
Baranov D.A., Yelenev V.D.
System of pressurization of the fuel tank of a launch vehicle using the heat of generator gas
Biryuk V.V., Smorodin A.V., Shepelev A.I., Onoprienko D.A.
Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control
Shorikov A.F., Kalev V.I.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Dynamic loading and questions of assuring the reliability of functioning of superheavy launch vehicle cryogenic pressure-operated valves
Sazanov V.P.
Analysis of the influence of low-orbit nanosatellite uncontrolled motion on the possibility of solving navigation and communication problems after its separation from the «Soyuz» carrier rocket upper-stage
Belokonov I.V., Kramlikh A.V., Timbai I.A.
Application of open-source software for industrial problems of vehicle lift-off gas dynamics
Abdurashidov T.O., Osipov A.V., Korchagova V.N., Kraposhin M.V., Smirnova Y.V., Strizhak S.V.
Mathematical model of investigating normal acoustic modes of launch vehicle modules
Popov P.A., Belov A.S., Kryuchkov A.N.
Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent
1 1., 1 1., 1 1., 1 1.
Selecting the conditions of nanosatellite separation from the upper stage of the arrier-rocket "Soyuz" in undirected flight
Avaryaskin D.P., Belokonov I.V., Timbay I.A., Lagno O.G.
Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments
Popov P.A., Sindyukov A.A., Malykhina O.I.
Peculiarities of solving three-dimensional problems of flow about a launch vehicle with large nose fairings using the ANSYS FLUENT software
Kharitonova A.N., Shakhov V.G.
Assessment of technicaland economical efficiency of developing carrier rockets with first-stage reusable units
1 1., 1 1.
Fluctuations of liquid fuel in tanks with oil recovery units
Dyachenko M.I., Duy Hung N., Temnov A.N.
Analysis of uncontrolled motion of the “ Soyuz “ carrier rocket orbital stage after payload separation
Belokonov I.V., Storozh A.D., Timbai I.A.
Assessing weight efficiency of carrier rockets launched from dirigibles and airplanes
Kurenkov V.I.
Frequency characteristics of a coaxial gas damper for booster feed line
Odinokov D.A., Gimadiyev A.G.
Principles of constructing systems and objects of a middle-class space rocket complex with increased load-carrying capacity
Baranov D.A., Yelenev V.D., Smorodin A.V.
Research of methods for protection the surface of cryogenic tanks from ice formation
1 1., 1 1., 1 1.
1 - 27 of 27 Items

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