Ejection unit for a satellite
US10569910B2 · kind B2 · utility
9Cited by
14References
11Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | May 9, 2017 |
| Grant date | Feb 25, 2020 |
| Priority date | — |
| Expiry date | Dec 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.