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.
Justification of the architecture of an interactive information model of the process of space-mission vehicle launch preparation
Privalov A.E., Bugaichenko P.Y.
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.
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.
Mathematical model of investigating normal acoustic modes of launch vehicle modules
Popov P.A., Belov A.S., Kryuchkov A.N.
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.
Fluctuations of liquid fuel in tanks with oil recovery units
Dyachenko M.I., Duy Hung N., Temnov A.N.
Procedure of designing a pilot operated gas pressure regulator for launch vehicle fuel tanks
Gimadiev A.G., Sverbilov V.Y., Stadnik D.M.
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.
Hard & soft complex for “Angara” family launch vehicles engine system development
Partola I.S.
History of small space vehicle progress and development at Plesetsk cosmodrome. Current problems of further development
Korotkov V.V., Vinogradov A.V.
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.
Determination of mass-power propertions for parametric range of launch vehicle modifications
Baranov D.A., Yelenev V.D.
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.
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.
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.
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.
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.
Dynamic loading and questions of assuring the reliability of functioning of superheavy launch vehicle cryogenic pressure-operated valves
Sazanov V.P.
On-stand emergency protection and control system for propulsion tests of «Soyuz-2-1B» launch vehicle
Liseykin V.A., Tozhokin I.A.
1 - 24 of 24 Items

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