Optimized Hybrid LSS for Middle Electrical Rockets Space Missions 981530
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.
Citation: Bartsev, S. and Okhonin, V., "Optimized Hybrid LSS for Middle Electrical Rockets Space Missions," SAE Technical Paper 981530, 1998, https://doi.org/10.4271/981530. Download Citation
Author(s):
S. I. Bartsev, V. A. Okhonin
Affiliated:
Institute of Biophysics SB RAS
Pages: 7
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Spacecraft
Radiation protection
Reliability
Biological sciences
Sun and solar
Optimization
Tools and equipment
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