Joint Optimization of the Thermal Control System and Cooled Instruments Characteristics 941376
The article is devoted to the problems of joint optimization of mass, power and reliability characteristics of the thermal control system and radio electronic instruments for long term mission spacecraft of high reliability requirements. The instrument operation reliability depending mainly on cooling medium temperature, the problem of optimum temperature level choice in the thermal control system taking into account the maintenance of the reliability required is of great interest.
The technique developed allows to choose the optimum instrument redundancy rate as well as the optimum temperature level in the thermal control system at minimum values of mass and power characteristics.
Citation: Malozemov, V., Kudriavtseva, N., and Alekseev, V., "Joint Optimization of the Thermal Control System and Cooled Instruments Characteristics," SAE Technical Paper 941376, 1994, https://doi.org/10.4271/941376. Download Citation
Vladimir V. Malozemov, Natalia S. Kudriavtseva, Vladimir A. Alekseev
COSMOS International Center for Advanced Studies Moscow Aviation Institute
International Conference On Environmental Systems
SAE 1994 Transactions: Journal of Aerospace-V103-1