Exoskeletal launch support structure

Patent metadata

Field	Value
Publication number	US-10633123-B2
Application number	US-201715480276-A
Country	US
Kind code	B2
Filing date	Apr 5, 2017
Priority date	Apr 5, 2017
Publication date	Apr 28, 2020
Grant date	Apr 28, 2020

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.

First claim

What is claimed is:

1. A system comprising:
a spacecraft including payload equipment, bus equipment and a secondary structure arrangement, each of the payload equipment and the bus equipment being coupled with the secondary structure arrangement; and
an exoskeletal launch support structure that provides a primary load path between a launch vehicle upper stage and the secondary structure arrangement; wherein
the spacecraft is configured to structurally interface with the launch vehicle upper stage only by way of the exoskeletal launch support structure;
the spacecraft is configured to deploy from the launch vehicle upper stage by separating from the exoskeletal launch support structure;
the exoskeletal launch support structure includes a first 3-D truss structure including at least four coupling nodes and at least six strut elements, attached together by a plurality of joints, each strut element disposed between and attached with a respective pair of the plurality of coupling nodes; and
the primary load path is the only load path between the secondary structure arrangement and the launch vehicle upper stage.

2. The system of claim 1 , wherein separating from the exoskeletal launch support structure results in substantially all of the exoskeletal launch support structure remaining with the launch vehicle upper stage.

3. The system of claim 2 , wherein:
the launch vehicle upper stage is disposed in a first orbit; and
the spacecraft includes an on-board propulsion subsystem configured to accomplish orbit raising of only the spacecraft from the first orbit to a second orbit.

4. The system of claim 1 , wherein the exo skeletal launch support structure interfaces with the secondary structure arrangement at a plurality of mounting hard points.

5. The system of claim 1 , wherein the secondary structure arrangement includes a 3-D truss structure configured to interface with the exoskeletal launch support structure.

6. A system comprising:
a plurality of spacecraft configured as a payload of a launch vehicle, each spacecraft including a respective secondary structure arrangement; and
an exoskeletal launch support structure that provides a primary load path between an upper stage of the launch vehicle and the respective secondary structure arrangements; wherein
the exoskeletal launch support structure includes a first 3-D truss structure including at least four coupling nodes and at least six strut elements, attached together by a plurality of joints, each strut element disposed between and attached with a respective pair of the plurality of coupling nodes; and
the primary load path is the only load path between the secondary structure arrangements and the launch vehicle upper stage.

7. The system of claim 6 , wherein each spacecraft is configured to deploy from the launch vehicle upper stage by separating from the exoskeletal launch support structure.

8. The system of claim 7 , wherein separating from the exoskeletal launch support structure results in substantially all of the exoskeletal launch support structure remaining with the launch vehicle upper stage.

9. The system of claim 8 , wherein
the launch vehicle upper stage is disposed in a first orbit; and
at least one of the plurality of spacecraft includes an on-board propulsion subsystem configured to accomplish orbit raising of the plurality of spacecraft from the first orbit to a second orbit.

10. The system of claim 8 , wherein
the launch vehicle upper stage is disposed in a first orbit; and
each of the plurality of spacecraft includes a respective on-board propulsion subsystem configured to accomplish orbit raising of a respective spacecraft from the first orbit to a respective second orbit.

11. The system of claim 6 , wherein the exoskeletal launch support structure interfaces with the respective secondary structures at a plurality of mounting hard points.

12. The system of claim 11 , wherein at least one of the respective secondary structures includes a 3-D truss structure configured to interface with the exoskeletal launch support structure.

13. A method for deploying a spacecraft from a launch vehicle upper stage disposed in a first orbit to a second orbit, the method comprising:
separating the spacecraft from an exoskeletal launch support structure; and
orbit raising the spacecraft from the first orbit to a respective second orbit; wherein
the spacecraft includes payload equipment and bus equipment and a secondary structure arrangement, each of the payload equipment and the bus equipment being coupled with the secondary structure arrangement;
the exoskeletal launch support structure provides a primary load path between a launch vehicle upper stage and the secondary structure arrangement and

the spacecraft is configured to structurally interface with the launch vehicle upper stage only by way of the exoskeletal launch support structure; and
the primary load path is the only load path between the secondary structure arrangement and the launch vehicle upper stage.

14. The method of claim 13 , wherein separating from the exoskeletal launch support structure results in substantially all of the exoskeletal launch support structure remaining with the launch vehicle upper stage.

15. The method of claim 13 , wherein the exoskeletal launch support structure includes a first 3-D truss structure including at least four coupling nodes and at least six strut elements, attached together by a plurality of joints, each strut element disposed between and attached with a respective pair of the plurality of coupling nodes.

Assignees

• Space Systems/Loral LLC

Inventors

• Chiang Jason

Classifications

• B64G1/002 Primary

  Launch systems · CPC title

• B64G1/403

  Solid propellant rocket engines · CPC title

• B64G1/645 Primary

  Separators · CPC title

• B64G1/405

  Operations & Transport · mapped topic

• B64G1/641

  Interstage or payload connectors (docking systems B64G1/646) · CPC title