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Joint Optimization of the Thermal Control System and Cooled Instruments Characteristics COSMOS International Center for Advanced Studies Moscow Aviation Institute

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Malozemov, Vladimir V., author.
Conference Name:
International Conference On Environmental Systems (1994-06-20 : Friedrichshafen, Germany)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1994
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
941376
Access Restriction:
Restricted for use by site license

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