Ascent trajectory, upper stage control system and spacecraft injection accuracy under Sea Launch Program
Автор: Gavrelyuk Оleg Petrovich, Kuptsova Irina Viktorovna
Журнал: Космическая техника и технологии @ktt-energia
Рубрика: Бортовые и наземные комплексы управления и системы
Статья в выпуске: 2 (5), 2014 года.
Бесплатный доступ
The ascent pattern and trajectory of a spacecraft to be launched into a target orbit by Zenit-3SL integrated launch vehicle under the Sea Launch program are described, some aspects of DM-SL upper stage control system operation are reviewed, the injection accuracy assessment is provided.
Launch point, ascent trajectory, upper stage, flight pattern, control system, injection accuracy, integrated launch vehicle, launch vehicle
Короткий адрес: https://sciup.org/14343444
IDR: 14343444
Статья научная
