Spacecraft servicing devices and related assemblies, systems, and methods

Patent metadata

Field	Value
Publication number	US-11724826-B2
Application number	US-202117476303-A
Country	US
Kind code	B2
Filing date	Sep 15, 2021
Priority date	Jul 21, 2017
Publication date	Aug 15, 2023
Grant date	Aug 15, 2023

Abstract

Spacecraft servicing devices and related methods may include a propellant tank configured to store a propellant and to be placed into fluid communication with a portion of the target spacecraft.

First claim

What is claimed is:

1. A spacecraft servicing system, comprising:
at least one deployable spacecraft servicing device comprising a propellant tank, the propellant tank configured to store at least one propellant and to be placed into fluid communication with a portion of a target spacecraft, the propellant tank configured to supply at least a portion of the at least one propellant to the target spacecraft during at least one servicing operation on the target spacecraft while being coupled to the target spacecraft, the at least one deployable spacecraft servicing device further comprising a propulsion device for independently moving the at least one deployable spacecraft servicing device and a coupling mechanism configured to couple the at least one deployable spacecraft servicing device to the target spacecraft, the propulsion device being attached to the at least one deployable spacecraft servicing device proximate the coupling mechanism; and
a host spacecraft comprising:
a body;
a propulsion system coupled to the body; and
a positioning mechanism coupled to the body, the host spacecraft configured to retrieve the at least one deployable spacecraft servicing device with the positioning mechanism and to transfer the at least one deployable spacecraft servicing device to the target spacecraft where the at least one deployable spacecraft servicing device is coupled to the target spacecraft in order to service the target spacecraft, the host spacecraft configured to remain in at least partial physical contact with the at least one deployable spacecraft servicing device until the at least one deployable spacecraft servicing device is coupled to the target spacecraft, the host spacecraft configured to cease physical contact with the at least one deployable spacecraft servicing device after the at least one deployable spacecraft servicing device is coupled to the target spacecraft.

2. The spacecraft servicing system of claim 1 , wherein the host spacecraft is configured to retrieve the at least one deployable spacecraft servicing device from a resupply device carrying a plurality of deployable spacecraft servicing devices at a location in space.

3. The spacecraft servicing system of claim 2 , wherein the host spacecraft is configured to rendezvous with the resupply device at the location in space and to transfer one or more of the plurality of deployable spacecraft servicing devices carried by the resupply device to the host spacecraft with the positioning mechanism.

4. The spacecraft servicing system of claim 1 , wherein the positioning mechanism comprises at least one external movable mechanism configured to deploy the at least one deployable spacecraft servicing device to the target spacecraft.

5. The spacecraft servicing system of claim 4 , wherein the at least one external movable mechanism comprises a robotic arm configured to deploy the at least one deployable spacecraft servicing device to the target spacecraft.

6. The spacecraft servicing system of claim 1 , wherein the host spacecraft is configured to install the at least one deployable spacecraft servicing device on the target spacecraft using only the propulsion system and the positioning mechanism of the host spacecraft.

7. The spacecraft servicing system of claim 1 , wherein the propulsion device of the at least one deployable spacecraft servicing device comprises a thruster assembly positioned on a boom extending outward from the at least one deployable spacecraft servicing device, the thruster assembly and the boom being rotatable about the at least one deployable spacecraft servicing device to maneuver the at least one deployable spacecraft servicing device.

8. The spacecraft servicing system of claim 1 , wherein the at least one deployable spacecraft servicing device is configured, when coupled to the target spacecraft, to supply the at least one propellant to the target spacecraft to alter at least one of an orbit or a velocity of the target spacecraft without refueling the target spacecraft.

9. The spacecraft servicing system of claim 1 , wherein the propulsion device the at least one deployable spacecraft servicing device comprises a thruster assembly positioned on a boom extending outward from the at least one deployable spacecraft servicing device, the thruster assembly and the boom being rotatable about the at least one deployable spacecraft servicing device to maneuver the at least one deployable spacecraft servicing device, the boom being attached to the at least one deployable spacecraft servicing device at the coupling mechanism.

10. The spacecraft servicing system of claim 1 , wherein the coupling mechanism is configured to modify the target spacecraft in order to place the propellant tank in fluid communication with a propulsion device of the target spacecraft.

11. The spacecraft servicing system of claim 1 , wherein the host spacecraft is configured to retrieve, transport, and deploy a plurality of deployable spacecraft servicing devices to at least one of a plurality of target spacecraft at one or more selected orbits in space.

12. The spacecraft servicing system of claim 1 , wherein the host spacecraft is configured to retrieve and/or refuel the at least one deployable spacecraft servicing device from the target spacecraft.

13. A spacecraft servicing system, comprising:
a host spacecraft; and
at least one spacecraft servicing device comprising a propellant tank, the propellant tank configured to store at least one propellant and to be placed into fluid communication with a portion of a target spacecraft, the propellant tank configured to supply at least a portion of the at least one propellant to the target spacecraft during at least one servicing operation on the target spacecraft while being coupled to the target spacecraft with a coupling device, the host spacecraft configured to retrieve the at least one spacecraft servicing device from a selected orbit in space and allocate the at least one spacecraft servicing device to a target spacecraft in order to supply the target spacecraft with the at least a portion of the at least one propellant of the propellant tanks of the at least one spacecraft servicing device, the at least one spacecraft servicing device further comprising a propulsion device for maneuvering the at least one spacecraft servicing device, the propulsion device being coupled to a body of the at least one spacecraft servicing device proximate the coupling device.

14. The spacecraft servicing system of claim 13 , further comprising a resupply spacecraft, the host spacecraft configured to retrieve the at least one spacecraft servicing device from the resupply spacecraft at the selected orbit in space.

15. The spacecraft servicing system of claim 13 , wherein the host spacecraft is configured to position the at least one spacecraft servicing device at a position in proximity to the target spacecraft, and wherein the at least one spacecraft servicing device comprises a coupling mechanism configured to engage with the target spacecraft at the position in proximity to the target spacecraft in order to secure the at least one spacecraft servicing device to the target spacecraft.

16. The spacecraft servicing system of claim 13 , wherein the host spacecraft configured to retrieve the at least one spacecraft servicing device from another spacecraft at the selected orbit in space.

17. The spacecraft servicing system of claim 13 , wherein the host spacecraft comprises a retrieval mechanism, the retrieval mechanism configured to engage and secure the at least one spacecraft servicing device in space for tran

Assignees

• Northrop Grumman Systems Corp

Inventors

• Nicholson James Garret
• Meyer Thomas Fred
• Guadagnoli Daniel

Classifications

• B64G1/2427

  Transfer orbits · CPC title

• B64G1/1078 Primary

  Maintenance satellites (refuelling in space B64G1/4024) · CPC title

• B64G1/646 Primary

  Docking or rendezvous systems (refuelling in space B64G1/4024) · CPC title

• B64G1/402

  Propellant tanks; Feeding propellants · CPC title

• B64G1/40

  Arrangements or adaptations of propulsion systems · CPC title