Aerospace
Technical Paper

Stand Rig Facility for Thermo-Vacuum Testing of Space Vehicles

2004-01-2309

07/19/2004

Event
International Conference On Environmental Systems
Authors
R. V. Gavrylov Special Research and Development Bureau of ILTP Nat. Acad. Sci. of Ukraine
Yu. A. Melenevskiy Special Research and Development Bureau of ILTP Nat. Acad. Sci. of Ukraine
V. I. Dranovskiy Yuzhnoye State Design Office
M. I. Koshkin Yuzhnoye State Design Office
Abstract
Content
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.
Meta Tags
Topics
Spacecraft
Radiation
Vacuum
Sun and solar
Hardware
Simulation and modeling
Affiliated or Co-Author
Special Research and Development Bureau of ILTP Nat. Acad. Sci. of Ukraine
Yuzhnoye State Design Office
Details
DOI
https://doi.org/10.4271/2004-01-2309
Pages
6
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.
Additional Details
Publisher
SAE International
Published
Jul 19, 2004
Product Code
2004-01-2309
Content Type
Technical Paper
Language
English