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Vol 23, No 3 (2024)

Selection of design parameters of a spacecraft electric propulsion engine ensuring the geostationary orbit raising mission

Kolesov A.V., Salmin V.V.

(Rus)

Vol 19, No 4 (2020)

Determination of loads on perforated tank partition

Filipov A.G., Glazkov I.E.

(Rus)

Vol 14, No 1 (2015)

Study of characteristics of the launch vehicle fuel line gas damper

Gimadiev A.G., Odinokov D.A., Stadnik D.M., Greshnyakov P.I.

(Rus)

Vol 10, No 2 (2011)

Determination of mass-power propertions for parametric range of launch vehicle modifications

Baranov D.A., Yelenev V.D.

(Rus)

Vol 12, No 3-1 (2013): Vestnik SSAU

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.

(Rus)

Vol 18, No 4 (2019)

Solving the problem of minimax closed-loop control of liquid-propellant launch vehicle fuel consumption control

Shorikov A.F., Kalev V.I.

(Rus)

Vol 14, No 1 (2015)

Vortex cleaning of fuel tank pressurant gas

Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.

(Rus)

Vol 9, No 4 (2010)

Dynamic loading and questions of assuring the reliability of functioning of superheavy launch vehicle cryogenic pressure-operated valves

Sazanov V.P.

(Rus)

Vol 12, No 4 (2013)

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.

(Rus)

Vol 16, No 4 (2017)

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.

(Rus)

Vol 11, No 4 (2012)

Mathematical model of investigating normal acoustic modes of launch vehicle modules

Popov P.A., Belov A.S., Kryuchkov A.N.

(Rus)

Vol 9, No 2 (2010): Special Issue

Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent

1 1., 1 1., 1 1., 1 1.

(Rus)

Vol 12, No 4 (2013)

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.

(Rus)

Vol 16, No 2 (2017)

Application of Bubnov-Galerkin method to determine fixed vibrational loads of launch vehicle compartments

Popov P.A., Sindyukov A.A., Malykhina O.I.

(Rus)

Vol 11, No 4 (2012)

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.

(Rus)

Vol 9, No 1 (2010)

Assessment of technicaland economical efficiency of developing carrier rockets with first-stage reusable units

1 1., 1 1.

(Rus)

Vol 16, No 2 (2017)

Fluctuations of liquid fuel in tanks with oil recovery units

Dyachenko M.I., Duy Hung N., Temnov A.N.

(Rus)

Vol 11, No 4 (2012)

Analysis of uncontrolled motion of the “ Soyuz “ carrier rocket orbital stage after payload separation

Belokonov I.V., Storozh A.D., Timbai I.A.

(Rus)

Vol 8, No 4 (2009)

Assessing weight efficiency of carrier rockets launched from dirigibles and airplanes

Kurenkov V.I.

(Rus)

Vol 16, No 1 (2017)

Frequency characteristics of a coaxial gas damper for booster feed line

Odinokov D.A., Gimadiyev A.G.

(Rus)

Vol 11, No 2 (2012)

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.

(Rus)

Vol 8, No 3-2 (2009): Special Issue

Research of methods for protection the surface of cryogenic tanks from ice formation

1 1., 1 1., 1 1.

(Rus)

Vol 15, No 4 (2016)

Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks

Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.

(Rus)

Vol 13, No 1 (2014)

Constructive actions for decreasing the acoustic pressure inside space-rocket products

Popov P.A., Sindyukov A.A.

(Rus)

Vol 8, No 1 (2009)

Determining flow regimes around rocket boosters on a part of the launch orbit

Kharitonova A.N.

(Rus)

Vol 15, No 1 (2016)

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.

(Rus)

Vol 10, No 2 (2011)

Promising technologies for solving boundary problems regarding the delivery of separating parts of carrier rockets with terminal targeting

Benevolsky S.V., Goncharenko V.I.

(Rus)

Vol 7, No 3 (2008): Special Issue

The process of ice formation on the surface of cryogenic tanks

Biryuk V.V., Shepelev A.I.

(Rus)

1 - 28 of 28 Items

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