Abstract: An orbit transition apparatus that transitions an orbit of a payload in outer space includes a rotating body, an adapter disposed on a center part of the rotating body for docking a payload, a launch module disposed outside of the rotating body for launching the payload, and a thruster for rotating the rotating body. The launch module may launch the payload to a target orbit.
Type:
Grant
Filed:
December 20, 2021
Date of Patent:
March 12, 2024
Assignee:
KOREA AEROSPACE RESEARCH INSTITUT
Inventors:
Sung Hyuck Im, Jun Seong Lee, Kee Joo Lee, Jae Sung Park