Публикации

 

Список статей, принятых к публикации в специальный выпуск Procedia Engineering

 

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Paper

Section

1

C. Bundesmann, C. Eichhorn, F. Scholze, D. Spemann, H. Neumann, F. Scortecci, H.J. Leiter, K. Holste, P.J. Klar, A. Bulit, K. Dannenmayer, J. Gonzalez del Amo

C. Bundesmann

Leibniz-Institute of Surface Modification

Advanced electric propulsion diagnostic tools at IOM

A-1

2

F. Scholze, C. Eichhorn, C. Bundesmann, D. Spemann, H. Neumann, A. Bulit, D. Feili, J. Gonzalez del Amo

F. Scholze

Leibniz Institute of Surface Modification (IOM)

Modelling of a Radio Frequency Plasma Bridge Neutralizer (RFPBN)

A-2

3

Yu Qin, Kan Xie, JiTing Ouyang

Kan Xie

Beijing Instituteof Technology

Measurements and Analysis of Potential Oscillations near the Hollow Cathode

A-3

4

V.А. Fedorov, А.I. Mogulkin, V.А. Obukhov, V.K. Abgaryan and V.V. Balashov

Mogulkin Andrej Igorevich

Moscow Aviation Institute

Numerical simulation of temperature deformation for radio frequency ion thruster electrodes

A-4

5

Stepan V. Kanev , Sergey A. Khartov , Vladislav V. Nigmatzyanov

Vladislav V. Nigmatzyanov

Moscow Aviation Institute

Analytical Model of Radio-Frequency Ion Thruster

A-5

6

Oleg Phylonin

Phylonin Oleg Vasilevich

Samara University

Methods and means of few projections tomographic diagnostics of ionic flows of KLA engines

A-6

7

Guanyu Zuo, Xiangyang Liu, Song Bai, Ningfei Wang, Zhiwen Wu, Kan Xie

Xiangyang Liu

Beijing Institute of Technology

Study on the Evolutionary Process of Characteristics of Plasma Properties in Pulsed Plasma Thruster

B-1

8

N. N. Antropov, A. V. Bogatyy, V.N. Boykachev, G.A. Dyakonov, N.V. Lyubinskaya, G.A. Popov, S.A. Semenikhin, V.K. Tyutin, V.N. Yakovlev

N. N. Antropov

Moscow Aviation Institute

Development of Russian next-generation ablative pulsed plasma thrusters

B-2

9

Antipov A.A., Bogatyy А.В.

A. A. Antipov

Moscow Aviation Institute

Simulation of motion of charged particles in an ablative pulsed plasma thruster at the initial stage of the discharge

B-3

10

O.V. Olshanskaya, A.U. Usanov

A.U. Usanov

EDB Fakel

Analysis of the SPT-140 thruster mechanical strength

B-4

11

R. Poddubniy

R. Poddubniy

EDB Fakel

Formation of the Items Surface Roughness from Noble Metals and Their Alloys to Increase Their Catalytic Capability

B-5

12

G.А. Parakhin, R.S. Pobbubniy, A.N. Nesterenko, A.P. Sinitsin

R. Poddubniy

EDB Fakel

Low-current Cathode With BaO Based Thermoemitter

B-6

13

P.A. Saevets, V.P. Kim, D.P. Grdlichko, P.G. Smirnov

P.A. Saevets

EDB Fakel

Investigation of low-power thruster on krypton propellant

B-7

14

D.A. Goza

D.A. Goza

EDB Fakel

Investigation of a hydroxylammonium nitrate thermocatalytic thruster on “green propellant”

B-8

15

V.М. Arbatskiy, S.V. Baranov, N.A. Vazhenin, A.P. Plokhikh, G.A. Popov

A.P. Plokhikh

Moscow Aviation Institute

Peculiarities of determination of electromagnetic interference emission from electric propulsion thrusters under ground conditions

C-1

16

Yu.V. Skvortsov, S.V. Glushkov, Chernyakin S.A.

Yu.V. Skvortsov

Samara University

The influence of space factors on the size stability of small spacecraft structure elements

C-10

17

Yu. V. Skvortsov, S. V. Glushkov, A. I. Aistov

Yu.V. Skvortsov

Samara University

Research on the low-cycle structural strength of the fuel tank membrane

C-11

18

Valery A. Komarov, Eugene I. Kurkin, Ramaz V. Charkviani

Eugene I. Kurkin

Samara University

Aerospace structures strength increasing using short fiber reinforcing

C-12

19

Valeriy A. Komarov, Alexander A. Pavlov, Svetlana A. Pavlova, Ramaz V. Charkviani

Svetlana A. Pavlova

Samara University

Reinforcement of Aerospace Structural Elements Made of Layered Composite Materials

C-13

20

Valeriy A. Komarov, Alexander A. Pavlov, Svetlana A. Pavlova

Valeriy A. Komarov

Samara University

Designing Additive Structures

C-14

21

Valery A. Komarov, Eugene I. Kurkin, Marie O. Spirina

Eugene I. Kurkin

Samara University

Composite aerospace structures shape distortion during all stages of vacuum infusion production

C-15

22

Nikolay Borgest, Anastasia Orlova

Anastasia Orlova

Samara University

Ontological Modeling Of Satellite’s Manufacturing Work Flow Instruction

C-16

23

Andrey V. Boldyrev, Dmitriy M. Kozlov, Maksim V. Pavelchuk

Andrey V. Boldyrev

Samara University

Evaluation of anisogrid composite lattice structures weight effectiveness using the load-carrying factor

C-17

24

Eugene I. Kurkin, Vladimir N. Samsonov, Valentin G. Shakhov

Eugene I. Kurkin

Samara University

Simulation of rarefied gas flows in microchannels

C-18

25

Ramaz V. Charkviani, Alexander A. Pavlov, Svetlana A. Pavlova

Svetlana A. Pavlova

Samara University

Interlaminar Strength and Stiffness of Layered Composite Materials

C-19

26

A.S. Filatyev, O.V. Yanova

O.V. Yanova

TsAGI

On the optimal use of electric ramjet for low-orbit spacecraft

C-2

27

E. I. Kurkin, V. O. Sadykova

Eugene I. Kurkin

Samara University

Application of short fiber reinforced composite materials multilevel model for design of ultra-light aerospace structures

C-20

28

Rumiya N. Kamalieva, Ramaz V. Charkviani

Ramaz V. Charkviani

Samara University

Creation of ultra-light spacecraft constructions made of composite materials

C-21

29

V. V. Salmin, S. I. Tkachennko, V. V. Volotsuev, I. V. Kaurov

V. V. Volotsuev

Samara University

Improving the efficiency of Earth monitoring mission by equipping small spacecraft AIST-2 with electric propulsion

C-3

30

S. I. Tkachenko, V. V. Salmin, I. S. Tkachenko, I. V. Kaurov, M. D. Korivin

M. D. Korivin

Samara University

Verifying parameters of ground data processing for thermal control system of small spacecraft AIST based on telemetry data obtained by Samara University's GCS

C-4

31

S. A. Ishkov, A. A. Khramov

A. A. Khramov

Samara University

Evaluation of Usage Efficiency of the Propulsion Systems with Energy Accumulation at Spacecraft

C-5

32

K. V. Petrukhina, A. S. Russkikh, V. V. Salmin, S. L. Safronov

A. S. Russkikh

Samara University

Shaping design layout of a combined insertion module with chemical acceleration and electric cruising units in creo elements/pro environment

C-6

33

Alexander Kucherov, Vladimir Kurenkov

A. Kucherov

Samara University

Use of cluster analysis for development of star tracker mass statistical model

C-7

34

A. I. Shulepov

A. I. Shulepov

Samara University

Placing of the onboard equipment of space vehicles with the account of influence of external factors

C-8

35

Sergey A. Ishkov

Sergey A. Ishkov

Samara University

Optimization of design parameters of spacecraft equipped with electro rocket low-thrust engine and calculation its applying area at low earth orbit

C-9

36

Mikhail Konstantinov, Min Thein

Mikhail Konstantinov

Moscow Aviation Institute

Preliminary Optimization of the Complicated Interplanetary Flight Path of the Spacecraft with Electric Propulsion

D-1

37

V. V. Volotsuev, V. V. Salmin, S. L. Safronov, V. V.Stratilatov, I. S. Tkachenko, S. S. Raube, S. V. Shikhanov, E. G. Shikhanova

S. V. Shikhanov

Samara University

Application of electric propulsion for low Earth orbit station keeping

D-10

38

Yu. M. Zabolotnov

Yu. M. Zabolotnov

Samara University

Dynamics of the formation of a rotating orbital tether system with the help of electro-thruster

D-11

39

Yevgeny Somov, Olga Starinova, Sergey Butyrin

Somov Evgenij Ivanovich

Samara State Technical University

Pulse-width Control of Electro-reaction Engines for a Station-keeping of  Land-survey  Satellite  on  Sun-synchronous  Orbit

D-12

40

Maxim K. Fain, Olga L. Starinova, Irina V. Gorbunova, Roman M. Khabibullin, Andrey Yu. Shornikov, Vyacheslav V. Kuptsov

Maxim K. Fain

Samara University

Simulation of low thrust spacecraft guided motion for a number of missions In the solar system

D-13

41

Maxim K. Fain

Maxim K. Fain

Samara University

Influence of the shaded areas on the low thrust spacecraft flight control in the Earth-Moon system

D-14

42

Olga L. Starinova,  Irina V. Gorbunova, Maxim K. Fain, Roman M. Khabibullin, Andrey Yu. Shornikov

Olga L. Starinova

Samara University

Application of electric propulsion for control spacecraft motion, which function on non Keplerian orbits

D-15

43

Mikhail Konstantinov, Victoria Svotina

Mikhail Konstantinov

Moscow Aviation Institute

Analysis for Feasibility of Spitzer’s Schemes Complication for Spacecraft Final Insertion into Geostationary Orbit by Electric Propulsion

D-2

44

V.G. Petukhov, Woo Sang Wook

V.G. Petukho

Moscow Aviation Institute

Joint optimization of the trajectory and the main parameters of electric propulsion system

D-3

45

V. V. Vorontsov, A. N. Kostin, A. S. Lovtsov, D. V. Volkov, Yu. M. Ermoshkin, E. N. Yakimov, O. A. Gorshkov, A. A. Ostapushchenko, D. V. Udalov, Yu. S. Arkhipov, S. A. Buldashev

Yu. M. Ermoshkin

JSC Academician M.F. Reshetnev
Information Satellite Sysyems

Development of KM-60 based orbit control propulsion subsystem for geostationary satellite

D-4

46

A.S. Lovtsov, D.A. Kravchenko

A.S. Lovtsov

State Scientific Centre Keldysh Research Center

Kinetic Simulation of Plasma in Ion Thruster Discharge Chamber. Comparison with experimental data

D-5

47

V. A. Soyfer, V. V. Salmin, S. V. Karpeev, A. S. Chetverikov, K. V. Peresypkin, I. S. Tkachenko

A. S. Chetverikov

Samara University

Insertion into geostationary orbit a spacecraft with diffractive orbit by low torque electric propulsion

D-6

48

S. A. Ishkov, K. V. Petrukhina, V. V. Salmin

V. V. Salmin

Samara University

Calculating launch windows for transfers of solar powered EP spacecraft between low-Earth non-coplanar circular orbits

D-7

49

V. V. Salmin, K. V.Petrukhina, A. S. Chetverikov

A. S. Chetverikov

Samara University

Optimizing ballistic schemes for transfer to geostationary orbits by electric propulsion

D-8

50

V.V. Salmin, K.V. Petrukhina, A.A. Kvetkin

A.A. Kvetkin

Samara University

Transfer of a satellite from high elliptical to geostationary orbit with the help of electric propulsion

D-9

51

Sergei Tkachenko, Vadim Salmin, Ivan Tkachenko, Sergei Safronov, Ivan Kaurov, Maksim Korovin, Sergei Volgin, Maksim Ivanushkin

Ivan Kaurov

Samara University

Experience in operating a constellation of AIST type small satellites with Samara University ground control center and perspective of managing a constellation of satellites using a distributed network of control centers based on multiagent approach

E-1

52

Igor Belokonov, Alexander Ivliev

Alexander Ivliev

Samara University

Development of a propulsion system for a maneuvering module of a low-orbit nanosatellite

E-2

53

Oleg Phylonin, Igor Belokonov

Oleg Phylonin

Samara University

The small-size ionic-plasma engine for nanosatellites

E-3

54

Oleg Phylonin, Igor Belokonov, Peter Nikolaev

Oleg Phylonin

Samara University

Control systems for the movement of nanosatellites in zone ISS

E-4

55

Sergey A. Ishkov, Gregory A. Filippov, Andrew A. Khramov

Gregory A. Filippov

Samara University

Autonomous Control Program for Special Spacecraft Debris Collector Rendezvous Transfer with Fragment of Space Debris with Low-Thrust

F-1

56

Sergey A. Ishkov, Gregory A. Filippov

Gregory A. Filippov

Samara University

Special refill spacecraft debris collector, equipped with electro rocket engine of low-thrust, design parameters optimization

F-2

57

Roman M. Khabibullin, Olga L. Starinova, Maxim K. Fain, Bakhyt N. Alipova, Hu Yudong

Roman M. Khabibullin

Samara University

The design of low thrust engine spacecraft for exploration of near-Earth asteroids

F-3

58

Andrey Shornikov, Olga Starinova

Olga Starinova

Samara University

Boundary problem solution algorithm for the task of controlled spacecraft's motion in irregular gravitational field of an asteroid

F-4

59

Andrey Shornikov, Olga Starinova

Olga Starinova

Samara University

Effectiveness analyses of electrospray sustainer engine installed on a spacecraft maneuvering in vicinity of an asteroid

F-5

60

Roman M. Khabibullin

Roman M. Khabibullin

Samara University

Comparison of solar sail spacecraft flight and
low thrust spacecraft flight to potentially hazardous asteroid orbit

F-6

61

Yu. M. Zabolotnov., V. V. Lyubimov, E. V. Kurkin

Yu. M. Zabolotnov

Samara University

Estimation of the perturbation when passing through the resonance of an asymmetric satellite with an electric propulsion

D-16