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Vol 12, No 1 (2013)

Modeling of mass spectrometers using linear and nonlinear ion mirrors

Syomkin N.D., Piyakov I.V., Rodin D.V.

(Rus)

Vol 17, No 4 (2018)

Propulsion systems and low-thrust rocket engines based on various physical principles for control systems of small and micro-spacecraft

Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 15, No 3 (2016)

Ion source of DMS-01 scientific equipment for «AIST no 2» small spacecraft

Semkin N.D., Piyakov I.V., Rodina M.A., Rodin D.V.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Optimal distribution of turboprop engine free energy between the screw and the jet with mass characteristics taken into account

Grigoriev V.A., Prokaev A.S.

(Rus)

Vol 10, No 7 (2011)

Gas mass spectrometer with a non-linear ion mirror

Pijakov I.V., Rodin D.V.

(Rus)

Vol 8, No 4 (2009)

Assessing weight efficiency of carrier rockets launched from dirigibles and airplanes

Kurenkov V.I.

(Rus)

Vol 19, No 1 (2020)

Optimal command control of hypersonic aircraft flight path in conditions of atmospheric disturbances

Krikunov M.M.

(Rus)

Vol 14, No 4 (2015)

Relationship between carbon concentration in a fuel and characteristics of flame propagation with a magnitude of ion current

Shaykin A.P., Budaev S.I., Galiev I.R.

(Rus)

Vol 11, No 2 (2012)

Assessing the efficiency of flights to high near-earth orbits using boosters with chemical and electro-rocket engines

Ishkov S.A., Fadeenkov P.V., Balakin V.L.

(Rus)

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

Motion trajectories of the vehicle with mass injection pre-compressor cooling turbojet engines as the first stage of aircraft-space systems

1 1., 1 1.

(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 18, No 3 (2019)

Disturbed motion of the hypersonic first stage of an aerospace system in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 17, No 4 (2018)

Analysis of control programs and flight paths of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 13, No 5-3 (2014): Special Issue

Estimation of mass-dimensional characteristics of a complex propulsion unit of earth remote sensing spacecraft

Kurenkov V.I., Kucherov A.S., Yakishik A.A.

(Rus)

Vol 11, No 1 (2012)

A hot-wire anemometric transducer of airflow mass rate

Nikolayev V.N.

(Rus)

Vol 8, No 2 (2009)

Statistical modeling of the process of serving the leaving passengers at the international Kurumotch airport

Romanenko V.A.

(Rus)

Vol 18, No 3 (2019)

Analytical determination of motion parameters of the center of mass of an uncooperative orbiter on the basis of measurement information provided by on-board systems of a space robot in a coplanar orbit

Ananenko V.M., Golyakov A.D., Kalabin P.V.

(Rus)

Vol 13, No 5-1 (2014): Special Issue

Assessing reduction gear mass in the problem of optimizing parameters of the working process of a turboprop engine at the initial design stage

Grigoryev V.A., Zagrebelnyi A.O., Prokaev A.S., Kuznetsov S.P.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Mixture modelling in a swirle flow in the ANSYS CFX program

Krasheninnikov S.V., Savchenko O.V.

(Rus)

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

Problems of heat and mass transfer on phase transformations or hemical reaction

Churkina N.V.

(Rus)

Vol 15, No 3 (2016)

Influence of fluctuation velocity on the electric conductivity of hydrocarbon flames

Shajkin A.P., Galiev I.R., Bobrovsky A.V.

(Rus)

Vol 11, No 7 (2012)

Method to improve accuracy mass measurement fluid in the tank

Solntseva A.V., Skvortsov B.V., Borminsky S.A.

(Rus)

Vol 12, No 1 (2013)

Determination of aircraft part masses based on a parametric 3D model at the stage of technical proposals

Borgest N.M., Gromov A.A., Tarabaeva A.I.

(Rus)

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

Energy sources in heat engine cycles

Mikheyenkov E.L.

(Rus)

Vol 15, No 1 (2016)

Influence of the suspension system on the accuracy of the aircraft modal testing results

Berns V.A., Dolgopolov A.V., Zhukov E.P., Marinin D.A.

(Rus)

Vol 11, No 4 (2012)

Stabilization of a pilot-operated gas pressure control valve by placing a throttle at the inlet

Stadnik D.M., Sverbilov V.Y., Makaryants G.M., Makaryants M.V.

(Rus)

Vol 12, No 3-2 (2013): Vestnik SSAU

Thermodynamic calculation of a thermomechanical compressor

Blagin E.V., Dovgyallo A.I., Uglanov D.A., Dostovalova S.S.

(Rus)

Vol 12, No 2 (2013)

Mechanisms of interaction of charged microparticles with the discharge electrode of the injector and the mass spectrometer target

Syomkin N.D., Vidmanov A.S., Bragin V.V.

(Rus)

Vol 10, No 3-2 (2011): Special Issue

Mixing processe research in 10…15 N thrusters

Salich V.L., Semkin E.V.

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

Studying the influence of the gas-dynamic non-stationary factors on the mathematical modelling of the gas turbine engines nonsetup work modes

Kofman V.M.

(Rus)

Vol 12, No 2 (2013)

Flame propagation velocity and ionization in burning gasoline and methane with addition of hydrogen

Shaykin A.P., Ivashin P.V., Galiev I.R.

(Rus)

Vol 20, No 2 (2021)

System of differential equations of aircraft spatial motion dynamics with arbitrary tensor of inertia and center of gravity position

Vereshchikov D.V.

(Rus)

Vol 18, No 2 (2019)

Disturbed motion of a hypersonic vehicle in climb

Balakin V.L., Krikunov M.M.

(Rus)

Vol 10, No 7 (2011)

Dust-impact mass-spectrometer for determination of elemental composition of micrometeorites and space debris particles

Piyakov I.V., Rodin D.V.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Volume and mass mathematical models of single-stage centripetal ultralow power turbines

Grigoriev V.A., Kalabukhov D.S., Rad'ko V.M.

(Rus)

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

Numerical investigation multifuel combustion gas turbine combustion chamber module

Malygina M.V.

(Rus)

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

Formation of microvortex gas flows in channels of a block catalyst with coplanar channels

Knysh Y.A., Tsibizov Y.I., Dmitriev D.N., Gorshkalev A.A.

(Rus)

Vol 19, No 2 (2020)

Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances

Krikunov M.M.

(Rus)

Vol 18, No 1 (2019)

Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system

Balakin V.L., Krikunov M.M.

(Rus)

Vol 14, No 4 (2015)

Methods and means of accelerating particles of natural and technogenic origin

Semkin N.D., Sukhachev K.I., Dorofeev A.S.

(Rus)

Vol 11, No 3-3 (2012): Special Issue

Formation in the channels of the block catalyst the micro vortex gas flows with intense twist

Knysh Y.A., Zibizov Y.I., Dmitriev D.N., Gorshkalev A.A.

(Rus)

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

The influence of swirling of a flow with axial countercurrent on the process of burning of hydrogenoxygen mix in the stream of water steam

Guryanov A.I., Vereshchagin I.M.

(Rus)

1 - 43 of 43 Items

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