Patent · US Active

Electrical umbilical system for space launch vehicle, using electromagnet

US12358653B2 · kind B2 · utility

0Cited by
3References
7Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 10, 2024
Grant dateJul 15, 2025
Priority date
Expiry dateSep 10, 2044

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64G1/002
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An electrical umbilical system for a space launch vehicle, using an electromagnet includes a connection module which is provided to a launch vehicle unit flyable by means of thrust; and an umbilical unit which is provided to a tower unit supporting the launch vehicle unit so as to stand upright, and which is capable of being electrically connected to the connection module. The umbilical unit includes a supply module which is capable of electrically connected to the connection module; a connection drive module which is coupled to the tower unit and connects the supply module to the connection module; a weight body which is coupled to the tower unit so as to be vertically movable; a drive line which connects the supply module and the weight body; and a guide roller which is rotatably coupled to the tower unit and supports the drive line.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.