Публикации
Список статей, принятых к публикации в специальный выпуск Procedia Engineering
№ |
Authors |
Corresponding author |
Organization |
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 |
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 |
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 |