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pro vyhledávání: '"Mojtaba Abolghasemi Najafabadi"'
Publikováno v:
Heliyon, Vol 10, Iss 6, Pp e27404- (2024)
The very low Earth orbit (VLEO), which includes orbits with altitudes of 100–450 km, has distinct advantages for remote-sensing spacecraft. Lower altitudes allow payloads with smaller dimensions, weight, and power to achieve performances similar to
Externí odkaz:
https://doaj.org/article/c4870867e7b54e569324c485a8b90f24
