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Title
Authors
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
Problems of testing and operation of hydraulic power transfer units
Polyakov N.A., Frolov G.K., Tselischev V.A., Tselischev D.V.
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.
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.
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.
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.
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.
Surging and auto-off the helicopter engine at start-up unguided missile from launchers
Prokopiev A.L., Povetkin O.V.
Determination of mass-power propertions for parametric range of launch vehicle modifications
Baranov D.A., Yelenev V.D.
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.
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.
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.
Inertial measuring units for future-generation aerospace products: fault-tolerance
Vodicheva L.V., Bel'skiy L.N., Parysheva Y.V., Lystsov A.A.
Oxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet
Ivanov A.I., Borisov V.A.
Assessment of technicaland economical efficiency of developing carrier rockets with first-stage reusable units
1 1., 1 1.
Computational and experimental research of exhaust gas treatment systems
Galevko V.V., Rakhmatov R.I.
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.
Unit impulse input tests of a system of the «Frigate» upper-stage rocket
Mikhalenkov N.A., Yermakov V.Y., Utkina Y.I.
Analysis of low-thrust liquid rocket engines with a methane air pump unit
Ivanov A.I., Kositsin I.P., Borisov V.A.
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.
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.
Thermal control of spacecraft star sensor attitude control system based on the solution of a coupled thermoelasticity problem
Tsaplin S.V., Bolychev S.A.
Increasing the overall performance of a two-stroke engine with spark ignition by fuel injection
Dovgyallo A.I., Krasheninnikov S.V., Shchepetov D.A.
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.
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.
System-simulator load the steering organs
Aliluev A.V.
1 - 26 of 26 Items

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