Stand rig facility for thermo-vacuum testing of space vehicles
Heading:
| 1Gavrylov, RV, 1Melenevsky, Yu.A, 2Konyukhov, SN, 2Dranovsky, VI, 2Koshkin, MI, 3Alekseev, Yu.S, 4Korotkov, AS, 4Schogol, VA, 4Sokolov, VA, 5Eremenko, VV, 3Komarov, VG, 3Makhonin, EI 1B.Verkin Institute for Low Temperature Physics and Engineering of the National Academy of Sciences of Ukraine, Kharkiv, Ukraine 2Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine 3State Space Agency of Ukraine, Kyiv, Ukraine 4The State Enterprise «Production Association Yuzhny Machine-Building Plant named after A.M. Makarov» (YUZHMASH), Dnipropetrovsk, Ukraine 5B.I. Verkin Institute for Low Temperature Physics and Engineering, NAS of Ukraine, Kharkiv |
| Kosm. nauka tehnol. 2004, 10 ;(5-6):042-046 |
| https://doi.org/10.15407/knit2004.05.042 |
| Publication Language: Russian |
Abstract: The stand rig facility for thermo-vacuum testing of space vehicles is described. It is intended for simulation of space vacuum, cold space environment, electromagnetic radiation of the Sun and Earth, and the Earth's albedo to determine the influence of those factors on thermal regime of hardware and instruments of the space vehicles.
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References:
1. Gavrilov R. V., Kislov A. M., Melenevsky Yu. A., Tserkovny A. I. The simulator of the Earth’s radiation for thermovacuum tests of spacecrafts. Kosm. nauka tehnol., 10 (5-6), 35—38 (2004) [in Russian]. 2. Gavrilov R. V., Kislov A. M., Romanenko V. G. Computer simulation of radiant fluxes in solar simulators. Kosm. nauka tehnol., 10 (5-6), 38—41 (2004) [in Russian].