Zobrazeno 1 - 1
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pro vyhledávání: '"continuation method by parameter"'
Autor:
Paing Soe Thu Oo
Publikováno v:
Космические аппараты и технологии, Vol 7, Iss 1, Pp 35-43 (2023)
A combined flight profile is being considered, in which the Falcon 9 launch vehicle launches the spacecraft into elliptical intermediate orbit from the Cape Canaveral launch site. In the process of analyzing the problem, the value of the height of th
Externí odkaz:
https://doaj.org/article/f21ec704d3db4a8187ee83bc55feeaf8