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Vol 22, No 3 (2023)

Bench tests of an electric engine-propeller group, as the first stage in the creation of a hybrid power plant

Sychev A.V., Ravikovich Y.A., Borisov D.A.

(Rus)

Vol 15, No 1 (2016)

Modeling orbital tether system deployment with limitations on the deployment speed

Ishkov S.A., Filippov G.A., Xiaoye X.

(Rus)

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

Building a diagnosis face gas dynamic seals

Falaleev S.V., Vinogradov I.S., Midyukin V.V.

(Rus)

Vol 7, No 3 (2008): Special Issue

Critical rotation frequency estimation of multispan rotors as rotors with elastic foundation

Petruhina N.P.

(Rus)

Vol 21, No 3 (2022)

Procedure of assessing the error of the device for measuring mass-centering and inertial characteristics of nanosatellites using reference objects

Vasin P.V., Barinova E.V.

(Rus)

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

Pilot study of frequency characteristics of an acoustic probe for measuring pressure pulsations in the gas turbine engine inlet device

Ivanenko V.N., Alexandrova T.G., Dyagileva E.C., Gimadiyev A.G., Bystrov N.D.

(Rus)

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

Investigation of structural damping of turbomashine blade vibrations using dynamic spin rigs

Nozhnitskiy Y.A., Fedina Y.A., Shadrin D.V.

(Rus)

Vol 12, No 1 (2013)

Unit impulse input tests of a system of the «Frigate» upper-stage rocket

Mikhalenkov N.A., Yermakov V.Y., Utkina Y.I.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Experimental research of thermal yet influence of staff LTRE upon the construction models of airspace devices

Shustov S.A.

(Rus)

Vol 14, No 3-1 (2015): Special Issue

New possibilities of using spin rigs to provide gas turbine engine strength reliability

Nozhnitsky Y.A., Fedina Y.A., Shadrin D.V., Servetnik A.N., Baluev B.A., Kanachkin A.V., Lepeshkin A.R., Tomashev A.A., Chernyshev S.A.

(Rus)

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

Methodical features of vibration tests of rotating blades using dynamic spin rigs

Nozhnitsky Y.A., Fedina Y.A., Shadrin D.V.

(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 10, No 3-4 (2011): Special Issue

Modernization of test-bench for small turbine-drives investigation

Matveev V.N., Shabliy L.S.

(Rus)

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

Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel

Ageenko Y.I., Lapshin E.A., Morozov I.I., Pegin I.V., Ryzhkov V.V.

(Rus)

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

About the probes for measuring pulsations of pressure in the flowing part gas turbine engines

Shorin V.P., Gimadiev A.G., Bystrov N.D., Ilinskij S.A.

(Rus)

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

Comparison of mass properties of high- pressure cylinders with cryogenic fill for a throttle cooling system

Dovgjallo A.I., Sarmin D.V., Uglanov D.A.

(Rus)

Vol 10, No 3-4 (2011): Special Issue

Test bench for investigation of thrusters intra-chamber working processes

Pervyshin A.N., Ryazanov A.I.

(Rus)

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

Automated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants

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

(Rus)

Vol 10, No 2 (2011)

Analysis of the applicability of laser stereolithography technology for the production of turbodrives

Shabliy L.S.

(Rus)

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

Turboprofan jet modeling and equivalent specific fuel consumption optimization subsystem construction on the seminatural modelling stand

Pogorelov G.I., Krivosheev I.A., Godovanyuk A.G., Danilin O.E., Badamshin B.I.

(Rus)

Vol 11, No 5-2 (2012): Special Issue

Stand for testing turbocharger rotor

Antipov V.A., Lazutkin G.V., Andrianov S.V., Velmin S.A.

(Rus)

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

Dynamic tests of probes for measurement of pulsations pressure at the raised average pressure

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

(Rus)

Vol 16, No 2 (2017)

Multi-purpose high-precision thermal vacuum testing bench and someresults of firing tests of non-hypergolic low-thrust rocket engines

Ryzhkov V.V., Verjasov Y.N., Galperin R.N., Gulyaev Y.I., Ivashin Y.S.

(Rus)

Vol 11, No 4 (2012)

Experimental verification of the specified characteristics of a solar battery at the stages of production and ground operation

Shuplyak Y.P., Sorokoletov V.I.

(Rus)

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

Firing test stand pulse detonation low-thrust engines

Govorenkho G.S., Teterin D.P., Kotelnikhov D.S., Aliluev A.V., Aliluev S.V., Fedorets V.N.

(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 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 8, No 1 (2009)

Experimental analysis of flow separation in low thrust rocket engine nozzles with a profiled supersonic part of the nozzle

Shustov S.A.

(Rus)

1 - 28 of 28 Items

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