Программа

Программа конференции на 25 августа 2016 г.

   

 

Sunday

28-Aug

Monday

29-Aug

Tuesday

30-Aug

Wednesday

31-Aug

Thursday

1-Sep

Friday

2-Sep

8:00

 

Breakfast

Breakfast

Breakfast

Breakfast

 

9:00

 

Plenary talks

Stay in Cheboksary

Stay in Nizhniy Novgorod

Technical session E

Breakfast

10:00

 

11:00

Excursion in Samara

Arrival in Samara

12:00

 

13:00

Lunch and break

Lunch and break

Lunch and break

Lunch and break

 

14:00

Technical session A

Technical session B1

Technical session C

Technical session F

 

15:00

Lunch

 

16:00

 

 

17:00

Welcome receptionon motor ship

Stay in Kazan

Technical session B2

Technical session D

Closing Ceremony

 

18:00

Departure from Samara

Gala dinner

 

19:00

Opening Ceremony

Stay in Makariev

 

20:00

Welcome dinner

Dinner

Dinner

 

21:00

 

 

 

Dinner

 

22:00

 

 

 

 

 

 

  

  

Plenary Talk

Title

Authors

Affilation

P1

Electric Propulsion in Germany: Present national activities, international cooperation and future vision

H.-W. Gronert-Marquardt,

M. L. Martin Perez

DLR

P2

German EP community – an overview on its activities inside the German Society for Aeronautics and Astronautics (DGLR) and presentation of the latest position paper

H. R. Neumann,

H.-P. Harmann,

A. Neumann,

H. J. Leiter

IOM Leipzig

P3

Cross-sectoral cooperation in the comprehensive study of ERE and their application: On the 50th anniversary of the “Yantar” Program

A. S. Filatyev, V. V. Skvortsov

TsAGI

 

 

Ion thrusters

(Technical Session A)

Title

Authors

Affilation

A1

Advanced electric propulsion diagnostic tools at IOM

C. Bundesmann, C. Eichhorn, 

F. Scholze, D.Spemann, H. Neumann, F. Scortecci, H. J. Leiter, K. Holste, P. J. Klar

Leibniz Institute of Surface Modification

A2

Modelling of a Radio Frequency Plasma Bridge Neutralizer (RFPBN)

F. Scholze, C. Eichhorn, C. Bundesmann, D. Spemann, H. Neumann

Leibniz Institute of Surface Modification

A3

Kinetic simulation of plasma in ion thruster discharge chamber

A. S. Lovtsov, 

D. Kravchenko

SSU FSUE Keldysh Research Centre

A4

Measurement of Forces in the Beam of Ion Sources and in the Plume of Sputter Targets

A. Spethmann, T. Trottenberg, H. Kersten

University of Kiel

A5

Analytical  Model of Radio-Frequency Ion Thruster

V. V. Nigmatzyanov, S. V. Kanev; Sergey A. Khartov

MAI

A6

High-performance digital-controlled radio-frequency generator for RF ion thrusters

J. Simon, U. Probst, P. J. Klar

University of Giessen

A7

Procedure of accelerated life tests of the ion thruster

R. V. Akhmetzhanov, V. V. Balashov, A. V. Bogatyy, D. A. Kashirin, 

V. A. Obukhov, G. A. Popov, M.V. Cherkasova, D.V.  Dukhopel’nikov,  S.G. Ivakhnenko, A.V. Kudryavtsev, A.I. Mogulkin,  E.V. Vorob’ev

 

MAI

A8

Temperature measurements in the low-power radio frequency ion thrusters

K. I. Kruglov, 

V. K. Abgaryan, 

R. V. Akhmetzhanov, 

V. V. Balashov, 

A. V. Bogatyy, 

A.I. Mogulkin

MAI

A9

Numerical simulation of temperature deformation for radio frequency ion thruster electrodes

A. I. Mogulkin, V.А. Fedorov, V.А. Obukhov, V.K. Abgaryan

MAI

A10

Methods and means of low angles projections tomography diagnostics of ionic streams engines of spacecraft

 

O. V. Phylonin

Samara University

A11

Application of additive manufacturing techniques to the production of ion optics

M. Lopez San Gregorio, K. Xie, N. Wang

Beijing Institute of Technology

A12

Update on diagnostics for DLR's electric propulsion test facility

A. Neumann

DLR

 

 

Stationary plasma thrusters 

(Technical Session B1)

Title

Authors

Affilation

B1.1

Assessment of the SPT-140 thruster mechanical strength

A. Y. Usanov, O. Boichenko

EDB Fakel

B1.2

Development of power processing unit for stationary plasma thruster of space vehicles on the basis of a modular distributed structure with a digital interface

M.B. Irz, S.V. Karamov, V.Y. Molotkov

AVECS JSC.

B1.3

Formation of the items surface roughness from noble metals and their alloys to increase their catalytic capability

R. S. Poddubniy

EDB Fakel

B1.4

Low-current cathode with BaO based thermoemitter

R. S. Poddubniy, G. Parakhin, A. Sinitsin

EDB Fakel

B1.5

Investigation of low-power thruster on krypton propellant

P. A. Saevets, 

V. P. Kim,

P. G. Smirnov, 

D. P. Grdlichko

EDB Fakel

B1.6

Investigation of the thermal catalytic thruster on HAN-based monopropellant

D. A. Goza

EDB Fakel

 

 

Magnetoplasmodynamic thrusters

(Technical Session B2)

Title

Authors

Affilation

B2.1

A review of European Electric propulsion plume modeling

 

B. Zitouni

OHB

B2.2

Measurements and analysis of potential oscillations near the hollow cathode

Y. Qin, K. Xie, J. Ouyang

Beijing Institute of Technology

B2.3

Development of next-generation ablative pulsed plasma thruster APPT-250

G. A. Dyakonov, N. N. Antropov, 

A. V. Bogatyi, V. N. Boykachev, 

N. V. Lyubinskaya, G. A. Popov, S. A. Semenikhin, V. K. Tyutin, V. N. Yakovlev

MAI

B2.4

Simulation of the charged particles motion in the discharge channel of the ablation pulsed plasma thruster

A. Antipov, A.V. Bogatyy

MAI

B2.5

Study on the evolutionary process of characteristics of plasma properties in pulsed plasma thruster

G. Zuo

Beijing Institute of Technology

 

 

Design of electric propulsion spacecraft, problems of power sources and thruster-spacecraft conjunction

(Technical Session C)

Title

Authors

Affilation

 

C1

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

A. S. Filatyev, O. V. Yanova

TsAGI

 

C2

The issues of the international standards development which are regulate methods and instruments of EPS development

V. Y. Sinelnikov, A. Semenkin, A. Sizov, V. Sinelnikov, E. Tverdokhlebova, T. Homin

TsNIIMash

 

C3

Iodine as an alternative propellant for Xenon

W. Gärtner, 

S. Scharmann, P. E. Köhler, K. Holste, 

P. J. Klar

University of Giessen

C4

The creation of a system of storage and supply of iodine in electricrocket thruster

P. A. Shcherbina,

V. G. Ostrovsky, A. A. Smolentsev

RSC Energia

 

C5

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

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

MAI

 

C6

Improvement of the “AIST-2D” satellite’s efficiency by equipping it with an electro-rocket vernier engine

V.V. Salmin, S.I. Tkachenko, I.S. Tkachenko, V.V. Volotsuev, S.L. Safronov, I.V. Kaurov, S.V. Shikhanov

Samara University

 

C7

Selection of the source data to create an energy system of low-orbit space vehicle with electrojet propulsion system

V. V. Volotsuev

Samara University

 

               

 

 

Problems of flight dynamics and motion control 

(Technical Session D)

Title

Authors

Affilation

D1

Development of orbit control propulsion subsystem on the base of KM-60 thruster for geostationary spacecraft

D. V. Volkov, Y. M. Ermoshkin, 

E. N. Yakimov

ISS-ReshetnevCompany

V. V. Vorontsov, A. N. Kostin,

A. S. Lovtsov

SSC FSUE Keldysh Research Centre

O. A. Gorshkov

Central Research Institute of Machine Building

A. A. Ostapushenko, 

D. V. Udalov

SPC Polus

Y. S. Arkhipov, 

S. A. Buldashev

Research Institute of Machine Building

D2

Optimization of heliocentric trajectories of spacecraft with a multimode electric propulsion

V. G. Petukhov, Woo Sang Wook

 

MAI

D3

An analysis of the expediency of complication of Spitzer’s scheme for SC insertion into geostationary orbit using electric propulsion

M. S. Konstantinov

MAI

D4

Application of electric propulsion for controled spacecraft, that function on non Keplerian orbits

O. L. Starinova, R. M. Khabibullin, M. K. Fain, I. V. Gorunova, A, Y. Shornikov

Samara University

D5

Keeping of parameters of a low working orbit of a space vehicle by means of electrojet engines

V. V. Volotsuev, V.V. Salmin, S. L. Safronov, I. S. Tkachenko

 

Samara University

N. R. Stratilatov, , S. S. Raube, S. V. Shihanov

JSC RSC “Progress”

D6

Application of electric propulsion for the insertion of the spacecraft with diffractive optical element in various positions of the geostationary orbit

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

Samara University

D7

Calculation of window start of a spacecraft with solar electric propulsion for flight between non-complanar near-earth circular orbits

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

Samara University

D8

Analyze of electric thruster efficiency for low Earth orbits correction problem

G. A. Filippov, S. A. Ishkov

Samara University

D9

Optimization of ballistic schemes flights spacecraft with electric propulsion power plants to the geostationary orbit

 

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

Samara University

D10

Forming a project of the combined module including a chemical upper stage and electric jet transport module in the programming environment CREO ELEMENTS/PRO

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

Samara University

D11

Delivery of a satellite with a highly elliptical orbit to geosynchronous orbit using electric propulsions

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

Samara University

D12

Analysis of the orbit injection scheme for a radiotelescope system with very long bases using EPS

I. V. Kaurov, V. V. Salmin, I. S. Tkachenko, S. L. Safronov, M. A. Ivanushkin, S. S. Volgin, M. D. Korovin

Samara University

D13

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

M. K. Fain

Samara University

 

 

Application problems of electric propulsion on the small, micro- and nano- satellites (Technical Session E)

Title

Authors

Affilation

E1

Radio-frequency ion thruster for microsatellites

D. A. Kashirin, N. N. Antropov,

R. V. Akhmetzhanov, A. V. Bogatyy, K. I. Kruglov, A. I. Mogulkin

 

MAI

E2

Experience in operating a constellation of small satellites using SSAU ground control center and perspectives of managing a constellation of satellites using a distributed network of control centers based on a multi-agent approach

S. I. Tkachenko, I. V. Kaurov, I. S. Tkachenko, M. A. Ivanushkin, S. S. Volgin, M. D. Korovin

Samara University

E3

Verification of the ground testing procedure of the thermal control system of “AIST” small satellite series using telemetry data obtained via Samara University ground control center

 

 

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

Samara University

E4

Analysis of power and thermal regime of an "AIST" series satellites for possibility of utilizing an EPS

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

Samara University

E5

Propulsion unit for maneuvering of the low-altitude nanosatellite

A. V. Ivliev, I. V. Belokonov

Samara University

E6

Control systems for the movement of nanosatellites in ISS zone

O. V. Phylonin, I. V. Belokonov, P. N. Nikolayev

Samara University

E7

The small size ions plasmas engine for nano satellites

O. V. Phylonin, I. V. Belokonov

Samara University

 

 

Electric propulsion application in planets and asteroid rendezvous mission and utilization of space debris

(Technical Session F)

Title

Authors

Affilation

F1

Special refill spacecraft debris collector, equipped with electric thruster, design parameters optimization

S. A. Ishkov, G. A. Filippov

Samara University

F2

Autonomous control program for special spacecraft debris collector rendezvous transfer with fragment of space debris

S. A. Ishkov, G. A. Filippov

Samara University

F3

Nonlinear flight simulation of low thrust spacecraft to asteroid orbit

R. M. Khabibullin

Samara University

F4

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

O. L. Starinova, A. Y. Shornikov

Samara University

F5

Modified Newton’s method as a boundary problem solution for the task of  controlled spacecraft's motion in dynamic gravitational field of an asteroid

O. L. Starinova, A. Y. Shornikov

Samara University

F6

The design of low thrust engine spacecraft for exploration of asteroids

O. L. Starinova, R. M. Khabibullin, M. K. Fain, H. Judon

Samara University

F7

Simulation of low thrust spacecraft guided motion for a number of missions in the Solar system

O. L. Starinova, I. V. Gorbunova, M. K. Fain, R. M. Khabibullin, A. Yu. Shornikov

Samara University

 

 

Poster presentations

Title

Authors

Affilation

1

Ontological modeling of flight preparation manual

N. M. Borgest, O. A. Orlova

Samara University

2

Aerospace structures strength increasing using short fiber reinforcing

V. A. Komarov, E. I. Kurkin, R. V. Charkviani

Samara University

3

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

V. A. Komarov, E. I. Kurkin, M. O. Spirina

Samara University

4

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

E. I. Kurkin, V. O. Sadykova

Samara University

5

Simulation of rarefied gas flows in microchannels

E. I. Kurkin, V. N. Samsonov, V. G. Shakhov

Samara University

6

Reinforcement of aerospace structural elements made of layered composite materials

S. A. Pavlova, A.A. Pavlov, R. V. Charkviani

Samara University

7

Creation of ultralight spacecraft constructions made of composite materials

R. V. Charkviani, R. N. Kamalieva

Samara University

8

Experimental study of interlaminar strength and stiffness of composite materials

S. A. Pavlova, A. A. Pavlov, R. V. Charkviani

Samara University

9

Evaluation of anisogrid composite lattice structures weight effectiveness

using the load-carrying factor

A. V. Boldyrev, D. M. Kozlov, M. V. Pavelchuk

Samara University

10

Designing of additive structures

V. A. Komarov, S. A. Pavlova, A. A. Pavlov

Samara University

11

Evaluation of usage efficiency of the propulsion systems with energy accumulation for the orbital correction

S.A. Ishkov, A. A. Khramov

Samara University

12

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

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

Samara University

13

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

Yu. M.Zabolotnov

Samara University

14

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

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

Samara University

15

Pulse-width control of electro-reaction engines for a station-keeping of land-survey satellite on sun-synchronous orbit

Y. I. Somov

Samara University