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Some Evaluation Methods and Measures for Overcoming the Thermal Non-Design Conditions During the Spacecraft Flight
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English
Abstract
The thermal non-design conditions, or off-nominal situations concerned with the disturbances in operation of the passive and active means of temperature control are considered in paper. The possibilities of using of simplified fast-acting method of thermal state analysis are shown in specific examples. There is described the procedure of heating the orbital station “Salut-6” after the power system failure. Other examples of non-design conditions are concerned with S/C “Venera” and “Sojuz”.
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Citation
Kopiatkevitch, R., Anfimov, N., and Surguchov, O., "Some Evaluation Methods and Measures for Overcoming the Thermal Non-Design Conditions During the Spacecraft Flight," SAE Technical Paper 941573, 1994, https://doi.org/10.4271/941573.Also In
References
- Anfimov N.A. 1991 Soviet Standard Software for Thermal Modeling of Spacecraft Fifth Thermal Workshop on ESATAN - FHTS and ESARAD 24-25 October 1991 Florence, Italy
- Designer Manual on Spacecraft Thermal Control 1989 2 184