FIELD: transport.
SUBSTANCE: invention relates to spacecraft (SC) motion control using solar radiation pressure forces distributed over SC working zones. The latter are formed as flat parallel optically transparent droplet flows. Distance between droplets of R radius in each flow in its lengthwise direction (Sx) and frontal-lateral direction (Sy) is divisible by
EFFECT: increase of efficiency of light pressure distributed external forces usage by means of decreasing their disturbing effect on relative SC motion.
3 dwg, 1 tbl
Title | Year | Author | Number |
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METHOD OF FORMING THRUST IN SOLAR RADIANT FLUX AND DEVICE FOR REALIZATION OF THIS METHOD | 2004 |
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RU2821815C1 |
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RU2209748C2 |
METHOD OF LIGHT-SAIL SPACECRAFT REORIENTATION AND THRUST CONTROL | 2011 |
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RU2480387C2 |
METHOD OF UNLOADING POWER GYROSCOPE SYSTEM OF SPACE VEHICLES | 1991 |
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RU2028256C1 |
METHOD TO GENERATE THRUST IN SOLAR RADIANT FLUX AND DEVICE TO THIS END | 2008 |
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RU2397923C2 |
Authors
Dates
2014-11-20—Published
2013-01-16—Filed