IP Library › Granted Patent US 11,623,770
Granted Patent B2
US 11,623,770 · App. 15/734,976 · Granted Apr 11, 2023

Spacecraft assembly arranged about a central axis and linked on longitudinal edges by fasteners

Inventors: Emmanuel Texier (Cannes la Bocca, FR); Yves Durand (Cannes la Bocca, FR); Jérôme Andy (Cannes la Bocca, FR); Pascal Ribeyron (Cannes la Bocca, FR); Julien Labarthe (Cannes la Bocca, FR)
Assignee: THALES
B64G1/641B64G2001/643
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Quick Facts
Patent No.
US 11,623,770
App. No.
15/734,976
Granted
Apr 11, 2023
Kind
B2
Abstract

An assembly includes at least one first collection of a plurality of spacecraft intended to be fastened to a launcher during a launch phase, wherein the spacecraft are arranged about a central axis (Z) in a given transverse plane perpendicular to the central axis, the spacecraft having edges along a longitudinal axis and being moreover arranged in such a way that a spacecraft is linked to a neighboring spacecraft of the collection by one edge by means of at least one fastener (B) positioned on the edge, so as to mechanically hold the spacecraft to one another, and a satellites-launcher adaptor to which the spacecraft are fastened in a transverse plane.

Claims (9)

1. A spacecraft assembly comprising:

at least one collection of a plurality of spacecraft configured to be fastened to a launcher during a launch phase,

wherein the plurality of spacecraft are arranged about a central axis transverse to said central axis,

each of the plurality of spacecraft having a plurality of edges along a longitudinal axis, and the plurality of spacecraft being arranged such that each spacecraft is linked to a neighboring spacecraft of the collection directly by a linking edge of said plurality of edges, linked by at least one fastener positioned on said linking edge, so as to mechanically hold said plurality of spacecraft to one another, and

a satellites-launcher adaptor to which said plurality of spacecraft are fastened along a transverse plane.

2. The spacecraft assembly as claimed in claim 1 , wherein the satellites-launcher adaptor is a part having a planar upper portion, on a spacecraft side, and a circular or conical lower portion, on a launcher side.

3. The spacecraft assembly as claimed in claim 1 , wherein the satellites-launcher adaptor is a cylindrical part located below the plurality of spacecraft.

4. The spacecraft assembly as claimed in claim 1 , comprising a central mast that is shared by all of the plurality of spacecraft and serves to control a sequence of release of the plurality of spacecraft.

5. The spacecraft assembly as claimed in claim 1 , comprising multiple collections of spacecraft, forming layers stacked along the central axis of the launcher.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 6, 2021
From: TEXIER, EMMANUEL; DURAND, YVES; ANDY, JÉRÔME; RIBEYRON, PASCAL; LABARTHE, JULIEN
To: THALES
Reel/Frame 054832/0166 →
Priority Claims (1)
FR 1800608 · Jun 14, 2018 · national
Continuity (1)
Related Publication 20210229839A1 · Jul 29, 2021