公开(公告)号：US20250091733A1

公开(公告)日：2025-03-20

申请号：US18827975

申请日：2024-09-09

Applicant: POSTECH RESEARCH AND BUSINESS DEVELOPMENT FOUNDATION

Inventor： Jeongrak LEE ,  Seonghyeon KIM ,  Anna LEE

IPC: B64G1/26 ,  B64G1/40

Abstract: A thruster for a micro-satellite according to an embodiment of the present disclosure includes a first thrust module configured to generate a first thrust in a first direction, a second thrust module configured to generate a second thrust in a second direction intersecting the first direction, and a control substrate on which the first thrust module and the second thrust module are mounted, the control substrate being configured to control the first thrust module and the second thrust module, in which the first thrust module and the second thrust module includes a plurality of printed circuit boards stacked.