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Optimized Hybrid LSS for Middle Electrical Rockets Space Missions Institute of Biophysics SB RAS

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Bartsev, S. I., author.
Conference Name:
International Conference On Environmental Systems (1998-07-13 : Danvers, Massachusetts, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1998
Summary:
The combination of electrical engines with solar arrays, well shielded against radiation long-term LSS, and remote control robot-manipulator system named "Space Rover" is shown to be very promising tool for space exploration. General parameters of space ship based on already developed components, and parameters of flight are considered. Optimal structure of hybrid LSS for middle space range space missions is calculated. As optimization criteria minimum mass and maximum reliability are chosen. Combinations of biological and physical-chemical components are evaluated. It is shown that namely hybrid LSS provide the highest level of reliability and the best mass parameters
Notes:
Vendor supplied data
Publisher Number:
981530
Access Restriction:
Restricted for use by site license

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