Design engineering and stability analysis of high precision mounting seats for small spacecraft “Aist-2D”

Бесплатный доступ

Information on creation of a design of the small spacecraft of remote sensing of Earth are provided. Results of development of design documentation, the vibrodynamic tests confirming construction consistency of the small spacecraft are presented. Experience of measuring of high precision mounting seats actual position is considered and analysed. Recommendations about further development of this technology are formulated.

Small spacecraft, it, construction consistency, vibrodynamic tests, measuring equipment

Короткий адрес: https://sciup.org/148205001

IDR: 148205001

Статья научная