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The problems of creating a propulsion system of a new generation supersonic passenger aircraft (review)
Alendar A.D., Lanshin A.I., Evstigneev A.A., Yakubovsky K.Y., Siluyanova M.V.
Calculation of optimum transfers from high-elliptic orbits to geostationary orbits using a stationary plasma engine
Kvetkin A.A., Kolesov A.V.
Verification of aero-engine numerical rotor models based on virtual static structural and modal tests
Shaposhnikov K.V., Degtyarev S.A., Leontiev M.K., Anisimov S.V.
The relevance of introducing a requirements management system in the production process of the aircraft engine construction industry
Malinovskiy I.M., Starodumov A.V., Myagkov K.A., Yusipov B.K.
Optimization of trajectory motion of the first stage of an aerospace system
Khramov A.A.
Peculiarities of starting a spark-ignition gas fuel internal combustion engine
Shishkov V.A.
Features of start-up the engine of internal combustion with spark ignition on gas fuel
Shishkov V.A.
Оptimization of gas turbine aircraft engine control throughout the engine service life
Gurevich O.S., Golberg F.D., Smetanin S.A., Trifonov M.E.
Analysis estimation of pulse jet engine operation in detonation mode
Seyfetdinov R.B., Seyfetdinov M.B., Gafurov S.A., Shakhmatov E.V.
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.
System-mathematical simulation of engine air hydraulic power supply
Goryunova N.R., Goryunov A.A.
Seal designing as element of aircraft engine systems and engine units
Vinogradov A.S.
Results of primary operation of NK-37 engine low emission combustion system
Bantikov D.Y., Yeliseev Y.S., Lavrov V.N., Pchelyakov A.A., Fedorchenko D.G., Tsybizov Y.I.
Estimation of the required thrust impulse for small spacecraft (SSC) control system with a propulsion system using fuel gas components
Titov B.A., Koltsov I.V.
Seal designing in a structure of the cooling system in gas turbine engine
Vinogradov A.S., Myatlev A.S.
Experimental studies of the components of high-frequency ion engine RD0310
Kazbanov A.A., Dronov P.A., Spivak O.O., Derkachev A.B.
Algorithm of adaptation of an electronic control system of internal combustion engines to various chemical compositions of gas fuel
Shishkov V.A.
Cycle parameters of an internal combustion spark-ignition gas piston engine with an electronic control system
Shishkov V.A.
Determining the angle of advance of ignition when switching from petrol to gas depending on fuel mixture burning rate
Shishkov V.A.
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.
Operation of an electronic system of control for spark-ignition gas fuel internal combustion engines in ignition misses
Shishkov V.A.
Research of the possibility of thermal conditions LREST using an infrared thermal imaging system
Ryzhkov V.V., Silyutin M.V.
Development and analysis of screw restrictor hydraulic characteristics in the air bleed valve control unit of a gas turbine engine
Gimadiev A.G., Makaryants G.M., Blyumin K.V., Dudnichenko I.M.
Hard & soft complex for “Angara” family launch vehicles engine system development
Partola I.S.
Research of the operability of an air-fuel lubrication and cooling system of gas turbine engine rotor bearings
Klimov V.N., Dud’ev D.Y., Sigaylo V.Y., Klimov N.I., Mashkov Y.K.
Fluctuations of pressure in rail gas injection of engines with spark ignition
Shishkov V.A.
Development of a procedure for the synthesis of a micro gas turbine engine neural controller with account for fuel consumption constraints
Kuznetsov A.V., Makaryants G.M.
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
Conversion of gas turbine engine oil system
Boev A.A., Grishanov O.A.
Modeling oil separation in the impeller of a radial-type centrifugal breather
Petrukhin A.G., Tryanov A.E.
Fulfilment of initial design level of gas turbine engine using the methods of «ASTRA» CAE system
Kuzmichev V.S., Krupenich I.N., Tkachenko A.Y.
Development of advanced low thrust rocket engines with ecologically friendly propellants
1 1., 1 1., 1 1.
Development of a virtual prototype of gasturbine engine at the stage of conceptual thermogasdynamic designusing the CAE-system «ASTRA»
Tkachenko A.Y., Krupenich I.N.
The usage of high power supply capacity transport spacecraft
Ivanovich S.N.
Assessment of gas turbine engine airfoil surface microstructure
Nosov N.V., Abramov A.D., Kosulin S.I.
Vortex cleaning of fuel tank pressurant gas
Biryuk V.V., Shimanov A.A., Onoprienko D.A., Smorodin A.V., Shepelev A.I.
Theoretical calculation approach of gas turbine engines compressor characteristic line
1 1.
About the thermal protection of the oil cavities for designing gas turbine engines
Tryanov A.Y., Grishanov O.A., Vinogradov A.S.
Internal combustion engine some cooling system components detailed calculation
Kolomin I.V., Ajukov A.A., Birjuk V.V.
Micro gas turbine engine imitation model
Kuznetsov A.V., Makaryants G.M.
Research of hydrodynamic processes in the lubrication system of gas turbine engines
Gulienko A.I., Shchurovskiy Y.M.
Computer-aided design of aircraft gas turbine engines and selection of materials for their main parts
Akhmedzyanov D.A., Kishalov A.E., Markina K.V.
Building foundations of virtual information-based educational environment
Zelenko L.S., Zagumennov D.A., Zinchenko A.O.
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.
Joint work of units and characteristics of elements gas the equipment for the engine of internal combustion with spark ignition
Shishkov V.A., Lesnih U.I.
On selection of automatic control system for crvogenic fuel gas turbine engine
Bukin V.A.
Using the «virtual engine» software in automatic control system of gas turbine engine
Golberg F.D., Gurevich O.S., Petukhov A.A.
Increasing the capacity of engine intake system
Kozin A.M., Rusakov M.M.
Experience in the development of 11Д58MФ liquid rocket engines
Smolentsev A.A.
Research of a seal work as an element of the air engine support
Vinogradov A.S., Rempel A.P.
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