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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.
Reducing energy consumption of vertical take-off and landing unmanned aerial vehicle using hybrid technical solutions
Lukyanov O.E., Hoang V.H., Komarov V.A., Nazarov D.V., Kurkin E.I., Quijada Pioquinto J.G., Chertykovtseva V.O.
Development of the method of calculation and design stand installation for testingmodes wet cleaning duct GTE
Silaev B.M., Malcev E.N.
Mathematical model of a generalized quadcopter kinematic scheme and its software implementation
Zelenskiy V.A., Kovalev M.A., Ovakimyan D.N., Kirillov V.S.
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.
Use of the methods of the structural programming to form the «reliability» diagrams of the fuel supply system of the gas turbine engines with the control elements failure order of no less than four
Smurova N.A.
Verification of energy efficiency of a low-thrust liquid-propellant engine with the deflector-centrifugal injecting pattern
Ageenko Y.I., Pegin I.V.
The choice of the kinematic scheme of formoobrazovany by stretch forming of obvodoobrazuyushchy covers of the difficult spatial form
Miheev V.A., Klochkov Y.S., Kuzina A.A., Grechnikova A.F., Savin D.V.
Rail line models for adaptive receiver track circuits
1 1.
Improvements in methods of analysis and control of space-rocket equipment reliability at the stage of complex electrical testing
Belova V.V.
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.
Choosing the mixing pattern for oxygen-hydrogen low-thrust rocket engines
Ryzhkov V.V., Morozov I.I.
Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency
Ageenko Y.I., Ilyin R.V., Pegin I.V.
Analysis and ballistic design of a medium-caliber system with an attached camera of accelerating
Safronov A.I., Azovsky V.M., Zorkin V.A., Chirkunova N.V.
Applying Lagrange’s approach to solving a one-dimensional problem of wave propagation in gas in linear formulation
Nikonov V.V., Shakhov V.G.
Method of calculating dynamic designs of space launch vehicles for designing systems of stabilization of their motion
Lobanov V.A.
Schemes, parameters, work process, characteristics and structure of long-range interception aircraft engines
Kovalev A.V., Sanin V.N., Krivenok A.G., Korolenko V.V.
50 n thrust correction engine for the "Luna-resurs" lunar module descent engine
Ageenko Y.I., Pegin I.V., Chesnokov D.V.
Structure of arterial blood pressure monitors
Fedotov A.A., Akulov S.A., Akulova A.S.
Hydrodynamic rinsing of hydrofuel system’ unflowing units
1 1.
Process of forming mirror-shaped relief plates of folded structure
Khaliulin V.I., Gimadiev R.S., Markovtsev V.A., Levshonkov N.V.
Construction of an upper stage flight pattern for placing a group of spacecraft into an orbit plane with the required angular distance between the satellites
Poplevin A.S., Panov N.A.
Analysis of models of fuel elements while using of surface mountng
Knyazeva G.N., Krasnoshchekova G.F., Tyulevin S.V.
Circuit design receipt autodynes signal to converter displacement parameters elements rotating parts of turbune unit
Danilin A.I., Gretskov A.A.
Project of 30 000 h.p. power gas turbine
Zrelov V.A.
Calculation of basic parameters of spring unloading and shock-proof devices of all-metal multicomponent dampfers on material МR basis
Lazutkin G.V., Parovay F.V., Petukhova M.A., Troynikov A.A.
Mathematical model of fuel sloshing in the measuring channel of the fuel expenditure control system
Kryukov Y.A.
Development liquid roket engine on component fuel liquefied natural gas and oxygen for reusable space launching systems
Efimochkin A.F., Khrisanfov S.P., Golubyatnik V.V., Kafarena P.V., Yeliseyev A.V.
Formation of the light field for linear movement of a microobject
Morozov A.
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.
Alignment and study of prototypes of the Offner hyperspectrometer
Karpeev S.V., Khonina S.N., Murdagulov A.R., Petrov M.V.
Investigation of the possibility of the creation LREST by thrust 400 N with a baffle - centrifugal scheme of NT and NDMG mixing
Ageenko Y.I., Ilin I.V., Pegin I.V., Shalamov E.A.
Analysis of on-board equipment robustness on the basis of COTS-products
Yefanov V.N., Bondarev A.V.
Comparative analysis of different approaches to designing thin-walled element structures of composite materials
Komarov V.A., Tchernyaev A.V.
The concept of generalized method of calculation and design of wet cleaning duct GTD
Silaev B.M., Malcev E.N.
Designing a model of mortgage lending for objects of spareholding housing construction
Korosteleva T.S.
Conceptually logical model of an integrated data system (software & hardware) for the control of individual and small-scale production of aviation components
Prilepsky I.V.
Design of schemes of financial and material flows in enterprise supply chains
Astapov S.V., Bogatyrev V.D.
Device for the assessment of surface condition by friction gaging
Kolpakov V.A., Kolpakov A.I., Ivliev N.A., Krichevsky S.V.
Increasing the energy efficiency of liquid rocket engine of small thrust (0,1-1,0) N with jet scheme of mixing
Nigodjuk V.E., Sulinov A.V.
Functional chart of a multichannel hydrologic-optical-chemical measuring complex and new measuring channels of hydrophysical parameters
Smirnov G.V., Olenin A.L.
Modelling of the sequential positive sequential scheme of formoobrazovany by stretch forming of obvodoobrazuyushchy covers of double curvature of the minimum nonuniform thickness
Miheev V.A., Klochkov Y.S., Kuzina A.A., Grechnikova A.F., Savin D.V.
Two models of rail lines for adaptive receiver track circuits
1 1.
Determination of aircraft part masses based on a parametric 3D model at the stage of technical proposals
Borgest N.M., Gromov A.A., Tarabaeva A.I.
1 - 44 of 44 Items

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