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Classification and comparative analysis of methods for limiting technogenic pollution in the near-Earth space
Klyushnikov V.Y., Zakharova A.P., Usovik I.V.
History of small space vehicle progress and development at Plesetsk cosmodrome. Current problems of further development
Korotkov V.V., Vinogradov A.V.
Stochastic method of investigating perturbed motion of a space vehicle in the atmosphere
Sokolov N.L.
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.
Basic aspects of topological technology of automated on-board equipment layout in space vehicle compartments using the example of “Yantar-2k” Earth remote sensing space vehicle
Belyakov A.A., Shulepov A.I.
On the acceptable level of risks in the implementation of strategic planning programs for technological innovations in the development of space systems
Petrukhin B.M., Bychkov Y.V., Letyagin A.A., Fursaeva T.V.
Development of a mathematical model of the internal structure of a granular heat accumulator for launching a mono-fuel gas generator
Zrelov V.A., Lykin A.Y.
Technical approach for estimation of engineering level of universal launch complexes for space launch vehicles witn use of overal parameter
1 1., 1 1., 1 1., 1 1.
Method of automated arrangement of devices in a spacecraft compartment taking into account connection to interface connectors of feed-through plates of an on-board cable system
Belyakov A.A., Prihodko V.I., Shulepov A.I.
Modern approach for design management in production enterprise integrated information space
Ivaschenko A.V., Kremenetskaya M.E., Filatov A.N., Peisakhovich D.G.
Analytical determination of motion parameters of the center of mass of an uncooperative orbiter on the basis of measurement information provided by on-board systems of a space robot in a coplanar orbit
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Locally optimal control of space tug motion between the libration points of the Earth-Moon system
Starinova O.L., Fain M.K.
Results of operation of scientific hardware «Space system of microacceleration compensation»
Semkin N.D., Piyakov I.V.
Building foundations of virtual information-based educational environment
Zelenko L.S., Zagumennov D.A., Zinchenko A.O.
Simulating electromagnetic field distribution due to electrostatic discharge on the spacecraft surface
Syomkin N.D., Balakin V.L., Bragin V.V.
Calculation of power dissipation in corps of onboard equipment of space vehicle in direct electrostatic discharge
Kostin A.V.
Methods of measurement and calculation of microaccelerations onboard of low orbit space microgravitational platform
1 1., 1 1., 1 1.
Dependence of the extent to which the space vehicle’s own atmosphere and plasma generated by stationary plasma engines affect the space vehicle on its structural lay-out
Testoyedov N.A., Smirnov V.A.
Choosing the form of space vehicle designed for descent in the rarefied atmosphere of Mars
Aslanov V.S., Ledkov A.S.
Design build process for the accuracy of eligibility
Grechnikov F.V., Tlustenko S.F.
Analysis of the accuracy of autonomous navigation of the space robot in the diagnosis of the technical condition of an orbital object
Golyakov A.D., Fominov I.V., Korolev S.Y.
The analysis of methods of protection of onboard equipment of space vehicles from influence of factors of the electrostatic discharge
Kostin A.V.
Information support of aviation embedded information and control systems lifecycle
Akimova T.E.
The influence of tether jamming on the motion of a space tether system during dynamic deployment
Ledkov A.S., Dyukov D.I.
Problems development of nuclear electric propulsion
Belogurov A.I., Kolbaya T.C., Rachuk V.S.
Through optimization of branching trajectories in view of random disturbances
1 1., 1 1.
Reputation of enterprises competing in the market from the point of view of consumers
Ivanov D.Y., Kirilina Y.V.
Integrated assessment of the efficiency of an orbital inspection space system based on small satellites
Tkachenko I.S., Kaurov I.V.
Influence of space vehicle remote power supply on thermal regimes of solar batteries
Steganov G.B., Beznyakov A.M., Nemirov A.V.
Optimization of space vehicle combined orbital plane change maneuver on the basis of pontryagin’s maximum principle
Khramov A.A.
Information control system for space experiments onboard international space station
Voronin F.A., Dunaeva I.V.
Dust-impact mass-spectrometer for determination of elemental composition of micrometeorites and space debris particles
Piyakov I.V., Rodin D.V.
Synthesis of dynamic modes of attitude motion of spacecraft with solid propellant rocket engine
Balakin V.L., Doroshin A.V., Krikunov M.M.
Choice of design parameters of universal platforms of small space vehicles
Volotsuev V.V., Tkachenko I.S., Safronov S.L.
Constructive actions for decreasing the acoustic pressure inside space-rocket products
Popov P.A., Sindyukov A.A.
analysis of demands on the evolution and development of new domestic booster population
1 1., 1 1.
Experiments aboard the space vehicle “Photon-M” NO.3 and some reseelts of the mission
Abrashkin V.I., Shatokhin S.M., Kovalyova T.B., Safronov S.L.
Contribution of the all-russian research institute of aviation materials to space exploration (1950-1980)
Bannikova N.F.
Deployment and stabilization of the motion of a space tethered system in a lunar orbit
Ledkova T.A., Zabolotnov Y.M.
Multi-satellite Universat-SOCRAT mission for monitoring technogenic and natural hazards
Sadovnichiy V.A., Panasyuk M.I., Lipunov V.M., Belov A.A., Bogomolov V.V., Garipov G.K., Gorbovskoi E.S., Iyudin A.F., Kalegaev V.V., Klimov P.A., Kornilov V.G., Mit S.K., Osedlo V.I., Petrov V.L., Podzolko M.V., Popova E.P., Rubinshtein I.A., Svertilov S.I., Tulupov V.I., Chepurnov A.S., Yashin I.V.
Efficiency of terminal control in the trans-atmospheric first stage of an aerospace system under atmospheric and aerodynamic disturbances
Balakin V.L., Kovalyov A.V., Krikunov M.M.
Development of the method of valuating the level of competitiveness of industrial enterprises working in the sphere of space-rocket engineering
Kirilina E.V.
Algorithms for the identification of star patterns in the task of correcting the inner orientation elements
Ivanov A.V., Pashentsev D.Y., Tishkin R.V.
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.
Problem of synthesis of a model for control and diagnostics in the manufacture of onboard equipment
Koptev A.N., Kirillov A.V., Yakovenko N.A., Dronov D.Y.
Solving the problem of stabilizing program deployment of an orbital tether system taking into account limitations on the rotary motion of the tip body
1 1., 1 1.
Modelling the architecture of a system controlling the condition of maintenance objects
Koptev A.N., Yergaliyev D.S., Sakhanov K.Z.
Experimental simulation of registration of outer space objects
Baryshev Y.Y., Syomkin N.D., Voronov K.Y.
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.
Optimization of space vehicle combined orbital plane change maneuver on the basis of the successive linearization method
Balakin V.L., Ishkov S.A., Khramov A.A.
Method of orthotransformation of space images in conditions of lack of cue
Spirin A.V., Rudnev N.I., Pastuh N.K., Shuklin I.I.
Choice of design characteristics of «garbage collector» spacecraft with a low-thrust electrojet engine
Ishkov S.A., Filippov G.A.
Peculiarities of Earth observation space vehicle control in contingencies
Akhmetov R.N., Makarov V.P., Sollogub A.V.
Dynamics of towing tethered spacecraft in the central gravitational field
Aslanov V., Yudintsev V.V.
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.
Vibration resistance problem for a space vehicle with single-degree-of-freedom powered gyroscopes
Filippov Y.I., Peresypkin K.V.
Structural model of individual forecasting of space radioelectronic equipment parameters
Tyulevin S.V., Piganov M.N.
The usage of high power supply capacity transport spacecraft
Ivanovich S.N.
Method of preliminary solution of the problem of space robot navigation by onboard astronomical measurements using the butterworth filter
Ananenko V.M., Golyakov A.D., Kalabin P.V.
Arrangement of data for the formation of a multidimensional array of essential insights in automated enterprise management system
Kartamyshev A.S.
Analysis of motion stability of a deployed space tether system with an atmospheric probe
Zhe D., Zabolotnov Y.M., Changqing W.
Accuracy control method for space complex products at the stage of design engineering
Yelenev V.D., Shuplyak Y.P.
The use of electric engine to reduce the microaccelerations level of space lab
Sedelnikov A.V., Sygurova E.Y., Kireeva A.A.
Visual approach to verifictaion of real-time control software
Tyugashev A.A., Bogatov A.Y., Shulyndin A.V.
System of artificial intellect support of low-thrust spacecraft interplanetary mission optimization
Starinova O.L.
Control over maintaining accuracy of integrity of reference surfaces of spacecraft components in their joint functioning at various stages of design
Yelenev V.D., Schuplyak Y.P.
Estimation of systematic errors in the results of navigational measurements with the use of spacecraft robot onboard facilities
Golyakov A.D., Richnyak A.M.
Technologies of reducing the technological environmental impact of space rocket launches
Shatrov J.T., Baranov D.A., Trushlyakov V.I., Kudentsov V.Y., Sitnikov D.V., Lempert D.B.
Calculation of the electromagnetic field in homogeneous hull of on board equipment of space vehicle under influence of electrostatic discharges
Kostin A.V.
Effect of shady areas orbit of damping natural oscillations of solar panels
Belousov A.I., Sedelnikov A.V.
Optimization methods of design-ballistic characteristics circumterraneous and interplanetary space vehicle with electrojet engines of low thrust
1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1., 1 1.
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.
Approximate methods of calculating optimal flights of space vehicles with low-thrust engines. Part II
Salmin V.V., Vassiliev V.V., Ishkov S.A., Romanenko V.A., Sokolov V.O., Starinova O.L., Yurin V.V.
Methods of validation of the ballistic structure of space surveillance system orbital segment
Fadin I.A., Yanov S.V., Samokhvalov O.A.
Iteration procedure of choosing a low-thrust rendezvous transfer control program in problems of space debris disposal in the geostationary orbit
Philippov G.A.
Small spacecraft for the registration of micrometeorites and space debris
Semkin N.D., Telegin А.М., Vidmanov A.S.
Cell suspensions status monitoring by bioimpedance method
Akulov S.A., Doroshenko R.J.
Method of production testing of electronic parts
Nasedkin A.V., Shumskikh I.Y.
Ways of the development of the radar space systems of the remote sensing of the Earth
1 1.
Process of autoreengineering of entreprise common information space
Ivashchenko A.V.
Orbital tether system motion equations considering space vehicle vibrations
Aslanov V.S., Stratilatov N.R.
1 - 81 of 81 Items

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