System and method of energy and mass transfer in low-gravity environments
A system and method for transferring energy and mass (supplies) in low-gravity environments. The system comprises a launcher and a receiver. The launcher hurls a capsule at a high velocity such that, when caught by the receiver, a portion of the kinetic energy of the launched capsule is converted to potential energy and stored. The stored energy is used at the receiver end for applications such as living habitats, mining operations, life-support systems, etc. In some instances, a portion of the initial energy is used to lob the capsule back, if desired. Launchers and receivers can be set up in different spatial configurations in a low-gravity environment such as in a circle with a centrally located launcher, a launcher downstream of a chain of receivers, or other configurations.
1. A system for energy and mass transportation, comprising:
a plurality of capsules;
a capsule launching mechanism comprising a first rotatable arm and a rotatable base, the first rotatable arm comprising a releasing mechanism on a first distal end and a receiving mechanism on a second distal end; wherein the capsule launching mechanism performs the steps of:
loading at least one capsule from the plurality of capsules into the first rotatable arm;
initializing rotation of the first rotatable arm; and
releasing the one capsule from the first rotatable arm; and
the capsule handling mechanism comprising a second rotatable arm; wherein the capsule handling mechanism performs the steps of:
catching the one capsule with the second rotatable arm; and
converting the kinetic energy from the one capsule as electric energy using regenerative braking.
2. The system of claim 1 , wherein the release mechanism and the receiving mechanism are the same mechanism.
3. The system of claim 1 , wherein the release mechanism is a passive release mechanism or an active release mechanism.
4. The system of claim 1 , wherein the capsule comprises a camera and a battery for terrain mapping.
5. The system of claim 1 , the rotatable base comprising a motor for creating movement in a transverse and longitudinal direction.
6. A system for energy and mass transportation comprising:
a plurality of capsules;
a capsule launching mechanism comprising a first rotatable arm and a rotatable base, the capsule launching mechanism is located on a spacecraft, the capsule launching mechanism further comprises a reaction wheel or thrusters configured to counteract the momentum of the releasing step wherein the capsule launching mechanism performs the steps of:
loading at least one capsule from the plurality of capsules into the first rotatable arm;
rotating the base;
releasing the one capsule from the first rotatable; and
the capsule handling mechanism comprising the second rotatable arm; wherein the capsule handling mechanism performs the steps of:
catching the one capsule with the second rotatable arm; and
converting the kinetic energy from the one capsule as electric energy using regenerative braking.
7. The system of claim 6 , wherein the capsule comprises a camera and a battery for terrain mapping.
8. The system of claim 6 , wherein the preparing step comprises matching a tangential velocity of the second rotatable arm with the velocity the one capsule to reduce to one capsule's impact force.
9. The system of claim 6 , wherein both the capsule launching mechanism and the capsule handling mechanism comprise a capsule creation and delivery system.
10. The system of claim 6 , wherein the capsule handling mechanism is located on a spacecraft, the capsule handling mechanism further comprises a reaction wheel or thrusters configured to counteract the momentum of the catching step.
11. A method for distributing energy in space, on the moon, or on Mars, comprising the steps of:
launching a capsule at a first velocity from a first rotatable arm, the first rotatable arm rotatable in a first plane and the first rotatable arm mounted to a rotatable base, the rotatable base rotatable in a second plane,
catching the capsule with a second rotatable arm, the second rotatable arm mounted to a second rotatable base,
converting kinetic energy from the catching step into electric energy using regenerative braking,
storing the electric energy, the stored energy comprising a first amount,
rotating the second rotatable base,
re-launching the capsule with the second rotatable arm at a second velocity, the second velocity lower than the first velocity, a second amount of energy used to re-launch the capsule being less than the first amount of stored energy.
12. The method of claim 11 further comprising the step of spinning the second rotatable arm at a rate such that a tangential velocity of a distal end of the rotatable arm matches the first velocity, the spinning step occurring prior to the catching step.
13. The method of claim 11 wherein the second rotatable arm never stops spinning between the catching step and the re-launching step.
14. The method of claim 11 wherein the first rotatable arm spins 360 degrees about a center axis.
15. The method of claim 14 , the first rotatable arm configured to release a capsule at a plurality of release angles.
16. The method of claim 11 , the launching step occurring on a spacecraft.
17. The method of claim 11 , the catching step occurring on a spacecraft.
18. The method of claim 11 , the capsule comprising a camera and a battery for terrain mapping.
19. The method of claim 11 , wherein the capsule launching mechanism is located on a spacecraft, the capsule launching mechanism further comprising a reaction wheel or thrusters configured to counteract the momentum of the releasing step.