Abstract: Today, chemical rockets are the most expensive components of a launch; even reusable boosters require costly fuel, ongoing maintenance, and long durations between launches. As a result, far too many space bound opportunities are prohibitively expensive. However, kinetic launchers offer an economical alternative for projecting payloads into orbit. Harnessing angular velocity, a centrifuge gradually accelerates its payload to hypersonic speeds within a vacuum sealed chamber; upon reaching the desired speed, its airlock opens and the payload is released into the atmosphere. Flux-Pinned Superconductors offer a radical advancement to this technology; wherein, Flux Pinning is used to levitate and stabilize the launch package while reinforcing the entire platform against centrifugal stress. These Flux-Pinned joints require no power, lubricant or physical contact, while providing limitless stiffness that is essentially impervious to mechanical wear.

Abstract: Today, chemical rockets are the most expensive components of a launch; even reusable boosters require costly fuel, ongoing maintenance, and long durations between launches. As a result, far too many space bound opportunities are prohibitively expensive. However, kinetic launchers offer an economical alternative for projecting payloads into orbit. Harnessing angular velocity, a centrifuge gradually accelerates its payload to hypersonic speeds within a vacuum sealed chamber; upon reaching the desired speed, its airlock opens and the payload is released into the atmosphere. Flux-Pinned Superconductors offer a radical advancement to this technology; wherein, Flux Pinning is used to levitate and stabilize the launch package while reinforcing the entire platform against centrifugal stress. These Flux-Pinned joints require no power, lubricant or physical contact, while providing limitless stiffness that is essentially impervious to mechanical wear.

Abstract: Here, we have devised a system that utilizes Flux-Pinning (or quantum locking) to provide Remote Structural Reinforcement to the rotor of a Flywheel Energy Storage System (FESS). This system utilizes superconducting materials to produce: (i) levitation of the rotor, (ii) a frictionless hinge to hold the rotor in place during operation, and (iii) a series of contactless quantum bonds that provide a reenforcing mechanism. This contactless reinforcement strengthens the rotor against centrifugal forces during operation. And ultimately, this system increases the tensile strength of the rotor; thereby increasing its maximum angular velocity (as well as the energy density of the FESS) without increasing the mass of the Rotor with additional reinforcement materials.

Abstract: The present invention relates to the production of edible wafers comprising (i) 100 parts by weight of a flour that comprises at least 5% by weight of the total flour of a non-wheat flour (such as millet; maize, barley, oats, rice, rye and/or soybeans) and/or at least 5% by weight of the total flour of a soluble fibre; (ii) an amount of water so the weight ratio of total amount of water to total amount of flour in the batter (denoted herein as R[w/f]) is no more than 1.5; and (iii) at least one enzyme comprising a cellulase in an amount of at least 0.0001 parts by weight; where the batter has a viscosity of from 200 to 1900 cps so it can be both pumped and baked on a heated surface without spillage. Preferably the flour has a low amount of (preferably is free of) gluten and/or gliadin proteins.

Abstract: The present invention relates to the production of wafers and more particularly to the use of a batter aerating system to obtain wafers with an effective density of at most 0.16 g/cm3, and with sufficient strength to be able to remove them from the wafer baking plates.

Abstract: The present invention relates to the production of wafers and more particularly to the use of a batter aerating system to obtain wafers with an effective density of at most 0.16 g/cm3, and with sufficient strength to be able to remove them from the wafer baking plates.