Patent · US Active

Reflector, deployable antenna, and spacecraft

US11381001B2 · kind B2 · utility

0Cited by
9References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 30, 2017
Grant dateJul 5, 2022
Priority date
Expiry dateApr 25, 2038

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64G1/425
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Deployable reflectors and antennas and spacecraft using such reflectors are disclosed. An example disclosed reflector includes: a hub having a cross-section formed in a circular, elliptical or polygonal shape; a plurality of ribs, each rib having an inner side surface facing an outer peripheral side of the hub when folded, and an outer side surface that is a surface opposite to the inner side surface, the plurality of ribs being folded to be wound around an outer periphery of the hub such that the inner side surface of each rib and the outer side surface of its adjacent rib partially face each other or the outer side surface of each rib and the inner side surface of its adjacent rib partially face each other, each rib being deployed in a parabolic shape; and a sheet installed across each of the plurality of ribs and capable of reflecting radio waves.

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