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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 9, No 2 (2010): Special Issue

Technical approach for estimation of engineering level of universal launch complexes for space launch vehicles witn use of overal parameter

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

(Rus)

Vol 18, No 3 (2019)

Justification of the architecture of an interactive information model of the process of space-mission vehicle launch preparation

Privalov A.E., Bugaichenko P.Y.

(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 9, No 2 (2010): Special Issue

Experimental determination of acoustic loads daunches of Strela LV and calculation of test modes for a spacecraft to be delivered by it to space

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

(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 1 (2011)

Definition of directions of developing methods, technical decisions and means of decreasing the technogenic influence on the environment for the omplementation on board of space launch vehicles

Shatrov Y.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y.

(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 13, No 5-4 (2014): Special Issue

11D58MF combined propulsion unit operating on oxygen-hydrogen fuel for an average-sized booster

Lupyak D.S., Smolentsev A.A., Sokolov B.A., Tumanin E.N., Tupitsin N.N.

(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)

On-stand emergency protection and control system for propulsion tests of «Soyuz-2-1B» launch vehicle

Liseykin V.A., Tozhokin I.A.

(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 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 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 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 15, No 1 (2016)

Technologies of reducing the technological environmental impact of space rocket launches

Shatrov J.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y., Sitnikov D.V., Lempert D.B.

(Rus)

Vol 10, No 3-1 (2011): Special Issue

Hard & soft complex for “Angara” family launch vehicles engine system development

Partola I.S.

(Rus)

Vol 8, No 4 (2009)

History of small space vehicle progress and development at Plesetsk cosmodrome. Current problems of further development

Korotkov V.V., Vinogradov A.V.

(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)

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

Baranov D.A., Yelenev V.D.

(Rus)

Vol 12, No 2 (2013)

Current state of the theory and practice of circuit wiring control and testing of the avionics of rocket fairings of middle-class launch vehicles

Koptev A.N., Gulyaev A.A.

(Rus)

1 - 25 of 25 Items

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