Optimization of the launch profile of geostationary spacecraft with electric propulsion system using Falcon-9 launch vehicle
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 the perigee and the inclination of the intermediate...
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| Format: | Article |
| Language: | Russian |
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Association «Technology Platform «National Information Satellite System»
2023-03-01
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| Series: | Космические аппараты и технологии |
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| Online Access: | http://journal-niss.ru/en/archive_view.php?num=297 |