Stand Rig Facility for Thermo-Vacuum Testing of Space Vehicles 2004-01-2309
The stand rig facility for thermo-vacuum testing of Space vehicles (STVT), described in this paper, is intended for simulation of: space vacuum, cold Space environment, electromagnetic radiation by the Sun and Earth, and Earth-albedo, as well as determination of influence of these factors on thermal regime of hardware and instruments of SV.
Citation: Gavrylov, R., Melenevskiy, Y., Dranovskiy, V., and Koshkin, M., "Stand Rig Facility for Thermo-Vacuum Testing of Space Vehicles," SAE Technical Paper 2004-01-2309, 2004, https://doi.org/10.4271/2004-01-2309. Download Citation
Author(s):
R. V. Gavrylov, Yu. A. Melenevskiy, V. I. Dranovskiy, M. I. Koshkin
Affiliated:
Special Research and Development Bureau of ILTP Nat. Acad. Sci. of Ukraine, Yuzhnoye State Design Office
Pages: 6
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Spacecraft
Radiation
Vacuum
Sun and solar
Hardware
Simulation and modeling
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