Abstract: Systems, methods, and devices of the various embodiments may provide a joint suitable for use with space systems, such as robotic space systems, (e.g., Extra Vehicular Activity (EVA) space systems, Intra Vehicular Activity (IVA) space systems, etc.), etc. Various embodiments provide a joint configured to enable structural connection of structural elements, such as trusses, antenna boom sections, beams, etc., including cantilevered elements. Various embodiments provide a joint configured to enable connection of truss structure sections. Various embodiments may provide a robotic erectable joint including an active joint half and a passive joint half configured to connect to the active joint half to thereby form the robotic erectable joint when so connected, wherein the robotic erectable joint has a noncircular cross section (e.g., polygon (e.g., square, triangle, hexagon, etc.) cross section, oval cross section, ellipse cross section, etc.).

Abstract: A manipulator includes first and second link arms which are connected together by a hinge. A cable actuation and tensioning system is provided between the link arms and includes a spreader arm, a driven element attached to each link arm and a cable engaged with the respective driven element and attached to the spreader arm. At least one of the arms, or all of the arms, can telescope to shorten or lengthen the arm(s) by movement of the system. The spreader arm may also be configured to slide relative to the first and second link arms to change the position of the spreader arm relative to the first and second link arms.

Abstract: A tension stiffened and tendon actuated manipulator is provided performing robotic-like movements when acquiring a payload. The manipulator design can be adapted for use in-space, lunar or other planetary installations as it is readily configurable for acquiring and precisely manipulating a payload in both a zero-g environment and in an environment with a gravity field. The manipulator includes a plurality of link arms, a hinge connecting adjacent link arms together to allow the adjacent link arms to rotate relative to each other and a cable actuation and tensioning system provided between adjacent link arms. The cable actuation and tensioning system includes a spreader arm and a plurality of driven and non-driven elements attached to the link arms and the spreader arm. At least one cable is routed around the driven and non-driven elements for actuating the hinge.

Abstract: A manipulator includes first and second link arms which are connected together by a hinge. A cable actuation and tensioning system is provided between the link arms and includes a spreader arm, a driven element attached to each link arm and a cable engaged with the respective driven element and attached to the spreader arm. At least one of the arms, or all of the arms, can telescope to shorten or lengthen the arm(s) by movement of the system. The spreader arm may also be configured to slide relative to the first and second link arms to change the position of the spreader arm relative to the first and second link arms.

Abstract: A tension stiffened and tendon actuated manipulator is provided performing robotic-like movements when acquiring a payload. The manipulator design can be adapted for use in-space, lunar or other planetary installations as it is readily configurable for acquiring and precisely manipulating a payload in both a zero-g environment and in an environment with a gravity field. The manipulator includes a plurality of link arms, a hinge connecting adjacent link arms together to allow the adjacent link arms to rotate relative to each other and a cable actuation and tensioning system provided between adjacent link arms. The cable actuation and tensioning system includes a spreader arm and a plurality of driven and non-driven elements attached to the link aims and the spreader arm. At least one cable is routed around the driven and non-driven elements for actuating the hinge.

Abstract: A tension stiffened and tendon actuated manipulator is provided performing robotic-like movements when acquiring a payload. The manipulator design can be adapted for use in-space, lunar or other planetary installations as it is readily configurable for acquiring and precisely manipulating a payload in both a zero-g environment and in an environment with a gravity field. The manipulator includes a plurality of link arms, a hinge connecting adjacent link arms together to allow the adjacent link arms to rotate relative to each other and a cable actuation and tensioning system provided between adjacent link arms. The cable actuation and tensioning system includes a spreader arm and a plurality of driven and non-driven elements attached to the link arms and the spreader arm. At least one cable is routed around the driven and non-driven elements for actuating the hinge.

Abstract: A tension stiffened and tendon actuated manipulator is provided performing robotic-like movements when acquiring a payload. The manipulator design can be adapted for use in-space, lunar or other planetary installations as it is readily configurable for acquiring and precisely manipulating a payload in both a zero-g environment and in an environment with a gravity field. The manipulator includes a plurality of link arms, a hinge connecting adjacent link arms together to allow the adjacent link arms to rotate relative to each other and a cable actuation and tensioning system provided between adjacent link arms. The cable actuation and tensioning system includes a spreader arm and a plurality of driven and non-driven elements attached to the link arms and the spreader arm. At least one cable is routed around the driven and non-driven elements for actuating the hinge.

Abstract: A payload lifter/manipulator module includes a rotatable joint supporting spreader arms angularly spaced with respect to one another. A rigid arm is fixedly coupled to the joint and extends out therefrom to a tip. A tension arm has a first end and a second end with the first end being fixedly coupled to the tip of the rigid arm. The tension arm incorporates pivots along the length thereof. Each pivot can be engaged by or disengaged from the outboard end of a spreader arm based on a position of the spreader arm. A hoist, positioned remotely with respect to the module and coupled to the second end of the tension arm, controls the position of the spreader arms to thereby control the position of the rigid arm's tip. Payload lifter/manipulator assemblies can be constructed with one or more of the modules.

Abstract: A payload lifter/manipulator module includes a rotatable joint supporting spreader arms angularly spaced with respect to one another. A rigid arm is fixedly coupled to the joint and extends out therefrom to a tip. A tension arm has a first end and a second end with the first end being fixedly coupled to the tip of the rigid arm. The tension arm incorporates pivots along the length thereof. Each pivot can be engaged by or disengaged from the outboard end of a spreader arm based on a position of the spreader arm. A hoist, positioned remotely with respect to the module and coupled to the second end of the tension arm, controls the position of the spreader arms to thereby control the position of the rigid arm's tip. Payload lifter/manipulator assemblies can be constructed with one or more of the modules.

Abstract: An animal feed which is improved by the addition of a nonviable antibiotic biomass. The biomass may be obtained by drying a fermented biomass of an organism capable of producing an antibiotic which is effective against mycotoxin contamination. The resultant animal feed is substantially free of fungal mycotoxin contamination.

Abstract: Post-hatch diseases in poultry caused by Dactylaria gallopava are prevented and treated by exposing the poultry environment to an effective quantity of natamycin.

Abstract: A method for marking a mask set to insure minimum mismatch between the masks when they are assembled into a set. Each mask in the set is evaluated against a known fixed standard, identified and marked such that when the set is assembled and utilized to produce an integrated circuit minimum mismatch between each element in each mask in the set will be realized.