Patent · US Active

Separation device for a spacecraft

US11932426B2 · kind B2 · utility

0Cited by
7References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 19, 2018
Grant dateMar 19, 2024
Priority date
Expiry dateJun 24, 2039

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16B21/165
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A separation device for a spacecraft or launcher, separation device being movable from a locked state, in which the separation device is arranged to lock onto a component of a spacecraft or launcher, to a released state, in which component is released, separation device including: an inner housing divided into at least two portions for locking onto component of spacecraft or launcher, and a locking arrangement arranged to move between a locking configuration and a releasing configuration, wherein the locking configuration is such that said at least two portions of inner housing are prevented from separating, wherein said locking arrangement includes: a first part arranged to at least partially enclose said at least two portions of inner housing when locking arrangement is in the locking configuration.

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