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Research of laws of interaction of components in a liquid phase self-igniting liquid rocket fuel

1 1., 1 1.

(Rus)

Diagnostics of state gas-fluid of flows in the field of cross vibration

Limanova N.I., Levkin U.S.

(Rus)

Vol 22, No 1 (2023)

Optimization of operation mode and design parameters of a finely-dispersed metallic liquid-alloy generator

Egorychev V.S., Ryazanov A.I., Khaimovich A.I.

(Rus)

Influence in a constructive and regime parameters antechamber by operation-in the combustion chamber liquid-propellant rocket engine thrusters on hypergolic liquid propellants

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 13, No 1 (2014)

Research of the mechanism of shock-inertial deposition of dispersed particles from a gas flow

Usmanova R.R., Zhernakov V.S.

(Rus)

Vol 22, No 2 (2023)

Influence of complex loading of radial bearings of the oscillation groups of liquid propellant engine steering gear on the frictional moment

Balyakin V.B., Lavrin A.V., Dolgikh D.E.

(Rus)

Vol 14, No 3-2 (2015): Special Issue

Methods of modeling the work process of hydrogen screw-centrifugal pumps using ANSYS CFD

Sulinov A.V., Shabliy L.S., Zubanov V.M.

(Rus)

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

Ways to improve the workflow of liquid rocket thrusters on hypergolic propellants

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 9, No 4 (2010)

Variations in free cross-sectional areas of the phases of double-phase flows under changes of gaseous phase rate of flow

Levkin Y.S.

(Rus)

Mixing parameters investigations and methods of approach to calculations and development of the thrusters with a spray-centrifugal scheme of NT and NDMH mixing on the confusion chamber wall in considered

1 1.

(Rus)

Vol 20, No 2 (2021)

Professor A.P. Merkulov’ role in the process of research and development of the vortex effect

Biryuk V.V., Lukachev S.V., Volov V.T., Pirallishvili S.A.

(Rus)

Research of the possibility of thermal conditions LREST using an infrared thermal imaging system

Ryzhkov V.V., Silyutin M.V.

(Rus)

Vol 15, No 4 (2016)

Peculiarities of the working process of low-thrust hypergolic-propellant liquid rocket engines with a thrust of less than 1 N

Nigodjuk V.E., Sulinov A.V.

(Rus)

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

CFD-modeling of processes in a high-pressure oxidizer pump for the turbopump assembly of a liquid rocket engine

Zubanov V.M., Shabliy L.S.

(Rus)

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

Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing

Ageenko Y.I., Ilin I.V., Pegin I.V., Shalamov E.A.

(Rus)

Vol 9, No 1 (2010)

Research of dynamics of initiation, propagation, growth and closure of bubble cavities and a supercavity in a pipe with decontaminated liquid under hydraulic impacts

1 1.

(Rus)

Obliteration’s problems in capillary-porous structures of aerospace hydro systems’ parts

1 1., 1 1.

(Rus)

Vol 19, No 4 (2020)

Development of improved performance electromagnetic valve for liquid rocket engine

Igolkin A.A., Chubenko T.A., Maksimov A.D.

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

Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency

Ageenko Y.I., Ilyin R.V., Pegin I.V.

(Rus)

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

Approaches to the evaluation of fuels for hypersonic engines

Sergeev S.M., Petrukhin N.V.

(Rus)

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

Experimental determination of the side forces acting on the combustion chamber in the altitude chamber at startup

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(Rus)

Vol 8, No 3-1 (2009): Special Issue

Investigation of friction joints working in nuclear plant with heat transfer medium consist of heavy high temperature liquid metal

Drozdov Y.N., Beznosov A.V., Makarov V.V., Puchkov V.N., Antonenkov M.A., Kuznetsov D.V.

(Rus)

Vol 19, No 1 (2020)

Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor

Shipov M.G., Steklova A.A., Davydov A.A.

(Rus)

Increasing the energy efficiency of liquid rocket engine of small thrust (0,1-1,0) N with jet scheme of mixing

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 15, No 4 (2016)

Efficiency of aft diffusers in vacuum systems of test benches for high-altitude firing tests of low-thrust liquid rocket engines

Galperin R.N., Gulyaev Y.I., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.

(Rus)

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

Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage

Kovalenko A.N., Pereverzev V.G., Marchan R.A., Blishun Y.V.

(Rus)

Vol 11, No 5-1 (2012): Special Issue

Stabilization of steady motions of a single rotor gyrostat with a cavity filled with a liquid of high viscosity

Alekseev A.V., Bezglasny S.P., Krasnikov V.S.

(Rus)

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

Experimental development of the LRE with CCCM nozzle’s extension

(Rus)

Vol 12, No 2 (2013)

Investigation of energy parameters of small-thrust liquid rocket engines with the geometric expansion ratio of the nozzle F=200

Ageenko Y.I., Nigodyuk V.E., Ryzhkov V.V., Sulinov A.V., Shustov S.A.

(Rus)

Vol 19, No 1 (2020)

Mathematical model of the “tank – nozzle” cooling system

Shalay V.V., Shcherban K.V.

(Rus)

Investigation of the kinetic properties of gas products of liquid-phase interaction hypergolic liquid rocket fuel

Nigodjuk V.E., Sulinov A.V.

(Rus)

Vol 10, No 7 (2011)

Investigation of factors affecting the accuracy of the flow rate of liquid, oil and gas

Plesovskikh K.Y.

(Rus)

Vol 11, No 4 (2012)

Modeling dynamic processes of response of fuel pressure-operated valves of superheavy launch vehicles in the tasks of providing structural strength

Sazanov V.P., Chirkov A.V.

(Rus)

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

Oxyhydrogen propulsion device base on water electrolysis and lrest on component H2 + O2 for control system SS

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

(Rus)

Enhancement of efficiency of casting processes in production of parts of aircraft engines by way of action of pulse-magnetic field on melt

Chernikov D.G., Glouschenkov V.A., Igolkin A.J.

(Rus)

Physical workflow model in the combustion chamber LREST with a jet-centrifugal jets on hypergolic propellants

Silyutin M.V., Shustov S.A.

(Rus)

Vol 14, No 3-2 (2015): Special Issue

Procedure of validated CFD-modeling of a two-stage screw-centrifugal pump

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

(Rus)

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

Research of influence of the thermal stream from the mid-flight liquid rocket engine on parameters of operating liquid rocket engines of small draught in the conditions of perspective razgonnogo's propulsion system of the block

Ageenko Y.I., Galperin R.N., Ivashin Y.S., Nigodjuk V.E., Ryzhkov V.V., Sulinov A.V.

(Rus)

Vol 13, No 1 (2014)

Analysis of nonstationary thermal state of a low-thrust liquid rocket engine taking into account injection, evaporation and combustion of liquid fuel droplets

Vorobiev A.G., Borovik I.N., Ha S.

(Rus)

Enhancement of efficiency of casting processes in production of parts of aircraft engines by way of action of pulse-magnetic field on melt

Chernikov D.G., Glouschenkov V.A., Igolkin A.J.

(Rus)

Vol 13, No 1 (2014)

Analysis of nonstationary thermal state of low-thrust liquid rocket engine with high-concentration hydrogen peroxide and kerosene propellant with film cooling

Vorobiev A.G., Borovik I.N., Ha S.

(Rus)

The flowing reactor as the tool of an experimental research of processes of transformation self-igniting liquid rocket fuel

1 1., 1 1.

(Rus)

Aspects of the numerical method calculating thermogazodynamic lrest based on not perfect passing of workflows in the combustion chamber

Silyutin M.V., Shustov S.A.

(Rus)

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

Experimental methods of carbon-based structures of nanotubs materials

Motova E.A., Moskvichev A.N.

(Rus)

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

Investigation of 11D428А-22 thruster operation dynamics with bellows flow stabilizer

Beshenev Y.A., Volkov A.V., Kazankin F.A.

(Rus)

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

Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet

Ivanov A.I., Borisov V.A.

(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)

Features of calculation of hydraulic characteristics of capillary spray jets of is liquid-stnyh rocket engines of small pull-rod

1 1., 1 1., 1 1.

(Rus)

Vol 20, No 4 (2021)

Selection of the optimum configuration and calculation studies of the parameters of a cryogenic propulsion system for an unmanned aerial vehicle

Tremkina O.V., Uglanov D.A., Urlapkin V.V., Korneev S.S., Komisar Y.V.

(Rus)