Zobrazeno 1 - 10
of 44
pro vyhledávání: '"V. G. Petukhov"'
Publikováno v:
Cosmic Research. 60:481-490
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dc1f28aa8a36a6d6e7859b3669688767
https://doi.org/10.1134/s0010952522050033
https://doi.org/10.1134/s0010952522050033
Autor:
Sung Wook Yoon, V. G. Petukhov
Publikováno v:
Cosmic Research. 59:517-528
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e6b57734ccd89e29cf0e5f13596be316
https://doi.org/10.1134/s0010952521060083
https://doi.org/10.1134/s0010952521060083
Autor:
Sung Wook Yoon, V. G. Petukhov
Publikováno v:
Cosmic Research. 59:401-413
The problem of optimization of perturbed trajectories of spacecraft with finite thrust is considered. The problem is solved using an indirect approach based on the application of the necessary optimality conditions in the form of the maximum principl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::62a8f68520d52c482ef02c70e984ef6f
https://doi.org/10.1134/s0010952521050099
https://doi.org/10.1134/s0010952521050099
Autor:
V. V. Riazanov, V. G. Petukhov
Publikováno v:
Известия Саратовского университета. Новая серия. Серия Математика. Механика. Информатика, Vol 21, Iss 2, Pp 202-212 (2021)
The work is devoted to the problem of towing space debris from a geostationary orbit to a graveyard orbit by a non-contact method using an ion beam created by the engine of an active spacecraft. For the planar case using the modified Hill task, the p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::638142ad518c22323a4a6437414b5992
https://doi.org/10.18500/1816-9791-2021-21-2-202-212
https://doi.org/10.18500/1816-9791-2021-21-2-202-212
Publikováno v:
Inorganic Materials: Applied Research. 11:861-864
The effect of the aviation fuel pumping rate on the electrostatic charging of filter papers treated with acrylic resin is studied. A model for predicting the electrostatic charging of the filter at various fuel pumping rates is developed. The pumping
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff74faf2c6d14aa2896a36553644a072
https://doi.org/10.1134/s2075113320040231
https://doi.org/10.1134/s2075113320040231
Autor:
V. G. Petukhov, A. V. Ivanyukhin
Publikováno v:
Cosmic Research. 57:378-388
The paper considers the problem of calculating direct and low-energy, low-thrust trajectories to the libration points of the Earth–Moon system and to halo-orbits. A method for solving the problem is proposed. It consists of calculating stable manif
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::109cd4122da719d5a924e12974035df6
https://doi.org/10.1134/s0010952519050022
https://doi.org/10.1134/s0010952519050022
Publikováno v:
Cosmic Research. 57:188-203
The problem of joint optimization of thrust vector control programs and main trajectory and design parameters of an interplanetary spacecraft with an electric propulsion system (EPS) is studied. The purpose of optimization is maximizing the useful sp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9bd83663dcc5be91906576360505e8f9
https://doi.org/10.1134/s0010952519030079
https://doi.org/10.1134/s0010952519030079
Autor:
V. G. Petukhov, Woo Sang Wook
Publikováno v:
Procedia Engineering. 185:312-318
The problem of joint optimization of the trajectory of a spacecraft with an electric propulsion system and for the main parameters of electric propulsion and power supply systems is considered. It is well known that for every space transportation ope
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::71e4af9379f66d37a08ecaf87e1fc824
https://doi.org/10.1016/j.proeng.2017.03.309
https://doi.org/10.1016/j.proeng.2017.03.309
Autor:
V. G. Petukhov, A. V. Ivanyukhin
Publikováno v:
Solar System Research. 50:552-559
The problem of optimizing the interplanetary trajectories of a spacecraft (SC) with a solar electric propulsion system (SEPS) is examined. The problem of investigating the permissible power minimum of the solar electric propulsion power plant require
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::88da8662fb3df8faa5c6bba910f75fc5
https://doi.org/10.1134/s0038094616070078
https://doi.org/10.1134/s0038094616070078
Publikováno v:
Russian Aeronautics (Iz VUZ). 58:286-291
In the paper, the problem whether it is possible to use an electro-rocket ramjet (ERRJ) thruster in a correcting propulsion system of a low-orbit spacecraft (SC) is analyzed. The calculated aerodynamic drag of the spacecraft is presented for orbits o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::875ae3e0a572efb24caa77622bbd981a
https://doi.org/10.3103/s106879981503006x
https://doi.org/10.3103/s106879981503006x