Rocket landing systems

Patent metadata

Field	Value
Publication number	US-11059610-B2
Application number	US-202016789222-A
Country	US
Kind code	B2
Filing date	Feb 12, 2020
Priority date	Apr 27, 2015
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

A rocket landing stabilization system can include one or more upright support structures such as posts, columns, or walls, from which one or more stabilizing elements can be supported. The stabilizing elements can be used to stabilize a rocket as it lands at a landing site. The rocket landing stabilization system can also include a cradle, funnel, or cone to catch or otherwise support a rocket as it lands at the landing site. The rocket landing stabilization system can be located on land or at sea.

First claim

The invention claimed is:

1. A rocket landing stabilization system, comprising:
a cradle sized to receive a landing rocket;
a stabilization structure positioned above the cradle; and
a body of water under the stabilization structure;
wherein the cradle floats on the body of water;
wherein the cradle is configured to be autonomously moved with respect to, and independently of, the stabilization structure.

2. The rocket landing stabilization system of claim 1 wherein the cradle includes at least one propeller to enable the cradle to be repositioned by the propeller.

3. The rocket landing stabilization system of claim 1 wherein the body of water is an artificial pond.

4. The rocket landing stabilization system of claim 1 wherein the cradle includes a first funnel and a second funnel below the first funnel.

5. The rocket landing stabilization system of claim 4 wherein the cradle includes a conically-shaped exhaust passage between the first funnel and the second funnel.

6. The rocket landing stabilization system of claim 5 wherein the cradle is configured such that exhaust from a rocket landing on the rocket landing stabilization system can flow from the rocket to the first funnel, through the first funnel to the conically-shaped exhaust passage, and through the conically-shaped exhaust passage out of the cradle.

7. The rocket landing stabilization system of claim 4 wherein the cradle includes a plurality of supporting plates coupled at respective first ends to the first funnel and at respective second ends opposite the first ends to the second funnel, such that the supporting plates extend vertically between the first and second funnels.

8. The rocket landing stabilization system of claim 4 wherein the cradle includes an upwardly-pointing cone positioned at a center of the first and second funnels.

9. The rocket landing stabilization system of claim 8 wherein the upwardly-pointing cone includes a plurality of openings through which water can be sprayed to cool exhaust from a rocket as the rocket lands on the rocket landing stabilization system.

10. A method of stabilizing a landing rocket, comprising:
landing the rocket on a cradle floating on a body of water;
actuating a stabilization structure positioned above the cradle and above the body of water; and
moving the cradle with respect to, and independently of, the stabilization structure.

11. The method of claim 10 wherein moving the cradle includes using at least one propeller to reposition the cradle.

12. The method of claim 10 wherein the body of water is an artificial pond.

13. The method of claim 10 wherein the cradle includes a first funnel and a second funnel below the first funnel.

14. The method of claim 13 wherein the cradle includes a conically-shaped exhaust passage between the first funnel and the second funnel.

15. The method of claim 14 wherein, as the rocket lands on the cradle, exhaust from the rocket flows from the rocket to the first funnel, through the first funnel to the conically-shaped exhaust passage, and through the conically-shaped exhaust passage out of the cradle.

16. The method of claim 13 wherein the cradle includes a plurality of supporting plates coupled at respective first ends to the first funnel and at respective second ends opposite the first ends to the second funnel, such that the supporting plates extend vertically between the first and second funnels.

17. The method of claim 13 wherein the cradle includes an upwardly-pointing cone positioned at a center of the first and second funnels.

18. The method of claim 17 wherein, as the rocket lands on the cradle, water is sprayed through a plurality of openings in the upwardly-pointing cone.

Assignees

• Knudsen N Eric
• Knudsen Matthew Niels
• Knudsen Andrew Niels
• Knudsen Jacob Niels

Inventors

• Knudsen N Eric
• Knudsen Matthew Niels
• Knudsen Andrew Niels
• Knudsen Jacob Niels

Classifications

• B64G5/00 Primary

  Ground equipment for vehicles, e.g. starting towers, fuelling arrangements (B64G3/00 takes precedence) · CPC title

• B64G1/625

  Landing devices; Undercarriages · CPC title

• B64G2005/005

  Systems for launching spacecraft from a platform at sea · CPC title

• B64G1/62 Primary

  Systems for re-entry into the earth's atmosphere; Retarding or landing devices · CPC title