The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Apr. 28, 2020

Filed:

Apr. 05, 2017
Applicant:

Space Systems/loral, Llc, Palo Alto, CA (US);

Inventor:

Jason Chiang, Fremont, CA (US);

Assignee:

Space Systems/Loral, LLC, Palo Alto, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64G 1/64 (2006.01); B64G 1/00 (2006.01); B64G 1/40 (2006.01);
U.S. Cl.
CPC ...
B64G 1/645 (2013.01); B64G 1/002 (2013.01); B64G 1/641 (2013.01); B64G 1/401 (2013.01); B64G 1/403 (2013.01); B64G 1/405 (2013.01); B64G 2001/643 (2013.01);
Abstract

A spacecraft includes payload equipment and bus equipment, each of the payload equipment and the bus equipment being coupled with a secondary structure arrangement. The spacecraft is configured to structurally interface with a launch vehicle upper stage only by way of an exoskeletal launch support structure (ELSS) that provides a first load path between a launch vehicle upper stage and the secondary structure arrangement. The spacecraft is configured to deploy from the launch vehicle upper stage by separating from the ELSS. In some implementations, the first load path is the only load path between the spacecraft and the launch vehicle upper stage, and substantially all of the ELSS remains with the launch vehicle upper stage. Because the secondary structure may be substantially less massy then the ELSS, subsequent orbit raising maneuvers may then be executed with a spacecraft having a reduced dry mass.


Find Patent Forward Citations

Loading…