公开(公告)号：US20240076064A1

公开(公告)日：2024-03-07

申请号：US17939290

申请日：2022-09-07

Applicant: Maxar Space LLC

Inventor： David Georgis ,  Frederick Oey ,  Robert Helmer

IPC: B64G1/42 ,  B64G1/10 ,  B64G1/50

CPC classification number: B64G1/428 ,  B64G1/1007 ,  B64G1/506

Abstract: An orbital satellite has a bus formed of a bus module and a payload module. Both the bus module and the payload modules may include a pair of panels integrally formed at an angle of for example 90° with respect to each other. Components and electronics supporting the satellite systems may be mounted on the panels of the bus and payload modules. Heat generated by the components and electronics are conducted between panels of the bus module and/or payload module. Sufficient heat transfer between panels occurs as a result of their being integrally formed with each other.