Patent · US Active

Ejection unit for a satellite

US10569910B2 · kind B2 · utility

9Cited by
14References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 9, 2017
Grant dateFeb 25, 2020
Priority date
Expiry dateDec 29, 2037

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64G1/6457
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

The invention relates to an ejection unit for at least one satellite, in particular a picosatellite, comprising a frame that defines an inner space for receiving the satellite; and a retention device for holding the satellite in the inner space, the retention device being configured such that the satellite is releasable from the retention device.

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