Описание
A 1U CubeSat developed for demonstrating the autonomous active attitude control capabilities based on magnetic actuation: in fact, the payload is an Active Attitude Determination and Control System. The commissioning phase foresees that the payload is deactivated leaving the satellite in its free tumbling motion, without any attitude stabilization. The A-ADCS starts its work when commanded from GCS, controlling the angular velocities and the attitude of the satellite. This program is being carried out at Politecnico di Torino by the AeroSpace System Engineering Team (ASSET). Aim of the project is the development and launch into orbit of the e-st@r satellite, which is a CubeSat class spacecraft. The project is entirely carried out by students, both graduate and undergraduate, under the supervision of researchers and professors.
NORAD ID/Int'l Code
41459/2016-025D
Ракета-носитель
Дата запуска/сведения/статус
2016-04-25/2024-05-09/Сведен
Производство
Группировка (серия)
Оператор (владелец)
Стоимость
Срок активного существования
Масса
1 kg
Масса сухая
Масса нагрузки
Габариты
Мощность
Тип (целевое назначение)
Технологический
Платформа
Разрешение
Полоса
Длины волн
Транспондеры
Пропускная способность
Емкость