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Vol 21, No 2 (2022)

Validation of the “stage – diffuser” system numerical study and its use for design modernization

Cherkasova M.G., Semakina E.Y., Chernikov V.A.

(Rus)

Vol 21, No 4 (2022)

Methodology of designing a space transport system including a “DM” chemical upper stage and an electric rocket transport module

Russkikh A.S., Salmin V.V.

(Rus)

Vol 15, No 4 (2016)

Analysis of low-thrust liquid rocket engines with a methane air pump unit

Ivanov A.I., Kositsin I.P., Borisov V.A.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

Investigation of the causes of the auger-centrifugal pump bearing destruction

Gafurov S.A., Rodionov L.V., Shahmatov E.V.

(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 19, No 4 (2020)

Choice of mission trajectory plans and conceptual design of electrical propulsion module for launching payloads into circumterrestrial orbits

Salmin V.V., Kvetkin A.A., Russkikh A.S.

(Rus)

Vol 15, No 3 (2016)

Efficiency of terminal control in the trans-atmospheric first stage of an aerospace system under atmospheric and aerodynamic disturbances

Balakin V.L., Kovalyov A.V., Krikunov M.M.

(Rus)

Vol 11, No 3-2 (2012): Special Issue

CFD modeling of air penetration into the fuel supply pipeline

Gafurov S.A., Rodionov L.V.

(Rus)

Vol 9, No 1 (2010)

Control programs and motion trajectories of hypersonic first stage of an aerospace system

1 1.

(Rus)

Vol 19, No 3 (2020)

Disturbed transatmospheric motion of the first stage of an aerospace system

Krikunov M.M.

(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 11, No 3-1 (2012): Special Issue

The analysis of real thermodynamic cycle of bypass engine with mixing

Medvedev V.V.

(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 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 15, No 1 (2016)

Selection of a nanosatellite group separation program for cluster launching from the «Soyuz» launch vehicle orbiter

Avaryaskin D.P., Shcherbakov M.S.

(Rus)

Vol 11, No 2 (2012)

Analysis of the causes of auger-centrifugal pump bearing destruction

Gafurov S.A., Rodionov L.V., Kryuchkov A.N., Makaryants G.M., Shakhmatov Y.V.

(Rus)

Vol 8, No 2 (2009)

Flight path of a supersonic aeroplane as the first stage of an aerospace system

Balakin V.L., Potapov V.I.

(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 10, No 6 (2011)

Nominal motion control program in a supersonic carrier aircraft

Balakin V.L., Potapov V.I.

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

Experience in the development of 11Д58MФ liquid rocket engines

Smolentsev A.A.

(Rus)

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

GTE parts optimal design

Temis Y.M., Yakushev D.A.

(Rus)

Vol 16, No 3 (2017)

Construction of an upper stage flight pattern for placing a group of spacecraft into an orbit plane with the required angular distance between the satellites

Poplevin A.S., Panov N.A.

(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)

Forming parts of the “atomizer” type for aircraft engines

Zvonov S.Y., Popov I.P., Mikheyev V.A.

(Rus)

Vol 15, No 4 (2016)

Simulation of the work process of a two-stage pump with a first-stage hydraulic drive

Matveev V.N., Shabliy L.S., Krivtsov A.V., Zubanov V.M., Ivanov A.I., Kositsin I.P., Baturin N.V.

(Rus)

Vol 13, No 5-2 (2014): Special Issue

Investigation of transformation of intermediate products of liquid-phase interaction propellant at the onset of combustion for rocket engine

Nigodjuk V.E., Sulinov A.V.

(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)

1 - 30 of 30 Items

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