Kinetic energy storage and transfer (KEST) space launch system

Patent metadata

Field	Value
Publication number	US-9260204-B2
Application number	US-201313963025-A
Country	US
Kind code	B2
Filing date	Aug 9, 2013
Priority date	Aug 9, 2013
Publication date	Feb 16, 2016
Grant date	Feb 16, 2016

Abstract

A Kinetic Energy Storage and Transfer (KEST) vehicle and target vehicle kinetic energy transfer method are provided. The KEST vehicle is configured to transfer kinetic energy to the target vehicle, propelling the target vehicle into a higher orbit or beyond the Earth. This is accomplished by a catching mechanism that contacts the target vehicle. The catching mechanism may also include a braking mechanism configured to accelerate the target vehicle, and thus slow the KEST vehicle, as the catching mechanism and target vehicle travel along one or more tethers of the KEST vehicle. Alternatively, the catching mechanism may be attached to an end of the one or more tethers and be configured to slow the target vehicle as the one or more tethers bend.

First claim

The invention claimed is:

1. A space vehicle, comprising:
an electric propulsion system;
at least one tether extending from the space vehicle; and
a catching mechanism that travels along the at least one tether, wherein
the braking mechanism is configured to accelerate the target vehicle, and slow the space vehicle, by applying a braking force as the catching mechanism and the target vehicle travel along the tether, thereby increasing kinetic energy of the target vehicle.

2. The space vehicle of claim 1 , wherein the braking mechanism comprises electromechanical brakes, electromagnetic brakes, or both.

3. The space vehicle of claim 1 , wherein
the catching mechanism is configured to contact a target vehicle, and
the braking mechanism is configured to accelerate the target vehicle, and slow the space vehicle, by applying a braking force as the catching mechanism and target vehicle travel along the tether, thereby transferring kinetic energy to the target vehicle.

4. The space vehicle of claim 3 , wherein the catching mechanism is further configured to release the target vehicle once a desired acceleration is reached.

5. The space vehicle of claim 4 , wherein the space vehicle is configured to place the target vehicle into a higher orbit or on a trajectory to leave Earth orbit.

6. The space vehicle of claim 1 , further comprising:
one or more solar arrays configured to provide power for the electric propulsion system.

7. The space vehicle of claim 1 , wherein the electric propulsion system is configured to place the apparatus into a higher orbit.

8. The space vehicle of claim 1 , wherein the at least one tether is 15,000 feet or more in length.

9. The space vehicle of claim 1 , wherein the catching mechanism comprises a grid of metal, fiber, or carbon fiber cables.

10. The space vehicle of claim 1 , wherein the at least one tether comprises a steel cable or a woven synthetic fiber cable.

11. The space vehicle of claim 1 , wherein
the catching mechanism comprises at least one braking mechanism, and
the at least one braking mechanism slows the space vehicle and accelerates a target vehicle contacted by the catching mechanism as momentum is incrementally transferred from the space vehicle to the target vehicle.

12. A space vehicle, comprising:
at least one tether extending from the space vehicle;
a catching mechanism configured to catch a target vehicle that travels along the at least one tether; and
a braking mechanism operably connected to the catching mechanism, the braking mechanism configured to slow the catching mechanism as the catching mechanism travels along the at least one tether, wherein
the catching mechanism comprises a braking mechanism configured to slow the catching mechanism as the catching mechanism travels along the at least one tether, and
the braking mechanism is configured to accelerate a target vehicle, and slow the space vehicle, by applying a braking force as the catching mechanism and the target vehicle travel along the tether, thereby increasing kinetic energy of the target vehicle.

Assignees

• Aerospace Corp

Inventors

• Hickman Robert Alan

Classifications

• B64G1/40

  Arrangements or adaptations of propulsion systems · CPC title

• B64G1/6462

  characterised by the means for engaging other vehicles · CPC title

• B64G1/006

  Reusable launch rockets or boosters · CPC title

• B64G1/4024

  refuelling in space · CPC title

• B64G1/411

  Electric propulsion · CPC title