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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 21, No 2 (2022)

3D investigation of heat exchange and hydrodynamics of high pressure turbine nozzle block platforms with different cooling schemes

Gorelov Y.G., Ananyev V.V., Zolotuhina D.A.

(Rus)

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

Experience in the development of 11Д58MФ liquid rocket engines

Smolentsev A.A.

(Rus)

Vol 16, No 3 (2017)

Computational and experimental research of exhaust gas treatment systems

Galevko V.V., Rakhmatov R.I.

(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 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 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 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 2 (2013)

Current state of the theory and practice of circuit wiring control and testing of the avionics of rocket fairings of middle-class launch vehicles

Koptev A.N., Gulyaev A.A.

(Rus)

Vol 15, No 2 (2016)

Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem

Tsaplin S.V., Bolychev S.A.

(Rus)

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

Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection

Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.

(Rus)

Vol 20, No 2 (2021)

Mathematical model of acoustic characteristics of polyurethane foam used for sound absorption in aerospace engineering

Kuznetsov A.V., Igolkin A.A., Safin A.I., Pantyushin A.O.

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

System-simulator load the steering organs

Aliluev A.V.

(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 10, No 6 (2011)

Motion of an upper stage rocket with a toroidal tank around the mass center in parameters of Cayley-Klein

Alekseev A.V., Krasnikov V.S.

(Rus)

Vol 13, No 1 (2014)

Allan variance-based assessment of basic characteristics of a strapdown inertial sensing unit

Kutovoy D.A., Sitnikov P.V., Fedotov A.A., Yakimov V.L.

(Rus)

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

Surging and auto-off the helicopter engine at start-up unguided missile from launchers

Prokopiev A.L., Povetkin O.V.

(Rus)

Vol 10, No 2 (2011)

Determination of mass-power propertions for parametric range of launch vehicle modifications

Baranov D.A., Yelenev V.D.

(Rus)

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

Application of technology microarc oxidation (mao) aluminum and titanium alloys to improve performance parts in engines

Krishtal M.M., Ivashin P.V., Polunin A.V.

(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 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)

Vol 17, No 1 (2018)

Inertial measuring units for future-generation aerospace products: fault-tolerance

Vodicheva L.V., Bel'skiy L.N., Parysheva Y.V., Lystsov A.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 9, No 1 (2010)

Assessment of technicaland economical efficiency of developing carrier rockets with first-stage reusable units

1 1., 1 1.

(Rus)

1 - 25 of 25 Items

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