Stand rig facility for thermo-vacuum testing of space vehicles

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.
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].