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Title
Authors
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.
Validation of the “stage – diffuser” system numerical study and its use for design modernization
Cherkasova M.G., Semakina E.Y., Chernikov V.A.
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.
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.
Analysis of possibility of residual propellant utilization in Soyuz orbital stage for controllable descent
1 1., 1 1., 1 1., 1 1.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
Investigation of the causes of the auger-centrifugal pump bearing destruction
Gafurov S.A., Rodionov L.V., Shahmatov E.V.
Assessment of technicaland economical efficiency of developing carrier rockets with first-stage reusable units
1 1., 1 1.
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.
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.
CFD modeling of air penetration into the fuel supply pipeline
Gafurov S.A., Rodionov L.V.
Control programs and motion trajectories of hypersonic first stage of an aerospace system
1 1.
Disturbed transatmospheric motion of the first stage of an aerospace system
Krikunov M.M.
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.
The analysis of real thermodynamic cycle of bypass engine with mixing
Medvedev V.V.
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.
Optimal command control of flight paths of aerospace system hypersonic first stage in conditions of atmospheric disturbances
Krikunov M.M.
Selection of a nanosatellite group separation program for cluster launching from the «Soyuz» launch vehicle orbiter
Avaryaskin D.P., Shcherbakov M.S.
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.
Flight path of a supersonic aeroplane as the first stage of an aerospace system
Balakin V.L., Potapov V.I.
Disturbed motion of the hypersonic first stage of an aerospace system in climb
Balakin V.L., Krikunov M.M.
Nominal motion control program in a supersonic carrier aircraft
Balakin V.L., Potapov V.I.
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.
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.
Analysis of control programs and climb paths of the hypersonic first stage of an aerospace system
Balakin V.L., Krikunov M.M.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
GTE parts optimal design
Temis Y.M., Yakushev D.A.
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.
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.
Forming parts of the “atomizer” type for aircraft engines
Zvonov S.Y., Popov I.P., Mikheyev V.A.
1 - 30 of 30 Items

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