Zobrazeno 1 - 10
of 10
pro vyhledávání: '"Irina V. Krainova"'
Publikováno v:
Heat Transfer Engineering. :1-16
Autor:
Irina V. Krainova, Dmitry L. Reviznikov, Evgeniy V. Chebakov, Ilia A. Nikolichev, Aleksey V. Nenarokomov, D.M. Titov, A. V. Morzhukhina
Publikováno v:
AIAA Journal. 60:2013-2027
A reliable control of current orientation of a spacecraft is a critical task in aerospace engineering, as the loss of the spacecraft’s attitude can endanger the whole mission. This makes it importa...
Autor:
Aleksey V. Nenarokomov, Dmitry L. Reviznikov, Irina V. Krainova, D.M. Titov, Evgeny V. Chebakov, A. V. Morzhukhina
Publikováno v:
Journal of Engineering Physics and Thermophysics. 92:948-955
At present, the angular position of small spacecraft is determined using solar sensors, magnetometers, and angular-velocity pickups as a rule, whereas star trackers are used for complicated problems requiring high accuracy. Each individual system has
Publikováno v:
Acta Astronautica. 160:323-330
The development of reliable thermal protected covering for optical research and control devices of satellites is a very important scientific and technical problem which demands providing a complex experimental-computational research of the correspond
A generalized analytical model for radiative transfer in vacuum thermal insulation of space vehicles
Autor:
Irina V. Krainova, Leonid A. Dombrovsky, Oleg M. Alifanov, S. A. Budnik, Aleksey V. Nenarokomov, D.M. Titov
Publikováno v:
Journal of Quantitative Spectroscopy and Radiative Transfer. 197:166-172
The previously developed spectral model for radiative transfer in vacuum thermal insulation of space vehicles is generalized to take into account possible thermal contact between a fibrous spacer and one of the neighboring aluminum foil layers. An ap
Autor:
Aleksey V. Nenarokomov, S. A. Budnik, Oleg M. Alifanov, Irina V. Krainova, Leonid A. Dombrovsky
Publikováno v:
International Journal of Numerical Methods for Heat & Fluid Flow. 27:598-614
Purpose The purpose of this study is to optimize multilayer vacuum thermal insulation (MLI) of modern high-weight spacecrafts. An adequate mathematical simulation of heat transfer in the MLI is impossible if there is no available information on the m
Autor:
Dmitry L. Reviznikov, Nishant Gaurav, Aleksey V. Nenarokomov, Andrey B. Nadiradze, D.M. Titov, S. A. Budnik, Irina V. Krainova, Evgeny V. Chebakov
Publikováno v:
Journal of Quantitative Spectroscopy and Radiative Transfer. 254:107174
A reliable control of current orientation of a spacecraft is a very important task in aerospace engineering. This makes important to elaborate a backup or replacement system which can be used for the verification or correction of the orientation. It
Autor:
Aleksey V. Nenarokomov, S. A. Budnik, D.M. Titov, Andrey B. Nadiradze, Irina V. Krainova, Evgeny V. Chebakov, Dmitry L. Reviznikov
Publikováno v:
Proceeding of Proceedings of the 9th International Symposium on Radiative Transfer, RAD-19.
Autor:
Leonid A. Dombrovsky, Dmitry L. Reviznikov, Irina V. Krainova, Evgeny V. Chebakov, Aleksey V. Nenarokomov
Publikováno v:
International Heat Transfer Conference 16.
Autor:
S. A. Budnik, Aleksey V. Nenarokomov, Oleg M. Alifanov, Leonid A. Dombrovsky, Irina V. Krainova
Publikováno v:
Proceedings of the 15th International Heat Transfer Conference.