CPC C07C 259/06 (2013.01) [A61P 35/00 (2018.01); B64G 1/1021 (2013.01); B64G 1/425 (2013.01); B64G 1/443 (2013.01); G01S 19/39 (2013.01); H04B 7/18513 (2013.01); H04B 7/195 (2013.01); B64G 1/1028 (2023.08); B64G 1/1035 (2023.08); B64G 1/66 (2013.01); G01S 13/90 (2013.01)] | 20 Claims |
1. A satellite configured to maintain an orbit between 100 km and 350 km, the satellite comprising:
a vehicle bus comprising a frontal section having at least one beveled surface configured to reduce drag; and
one or more stabilization surfaces mounted to and extending outwardly from the vehicle bus,
wherein the one or more stabilization surfaces and the at least one beveled surface comprise a material selected to at least partially specularly reflect incident atmospheric air particles during flight, wherein the material comprises SiOx, and
wherein the material and the at least one beveled surface reduce drag on the satellite.
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