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A deployable truss with modified primary orthogonal joints. The construction of these joints causes the center-hinged primary chords on opposite sides of a truss bay to fold inward in a plane orthogonal to the folding planes of the side diagonals while the two secondary chords fold in planes orthogo

A deployable truss with modified primary orthogonal joints. The construction of these joints causes the center-hinged primary chords on opposite sides of a truss bay to fold inward in a plane orthogonal to the folding planes of the side diagonals while the two secondary chords fold in planes orthogonal to the plane of the in-folding primary chords. This provides for stiffness and stability during deploy and retract. The unique joint configuration permits the truss to deploy one bay at a time in a stable manner while having lateral bending stiffness, and the truss thus can extend and retract in a sequential manner. It can deploy integral flat panels nested between the secondary folding chords, or use cross bracing in lieu of panels. The truss can be triangular, square or rectangular in cross-section. A powered support frame may be used in conjunction with the truss.

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1. A deployable truss, comprising: at least two primary chords, said primary chords comprising a plurality of primary chordal members connected end-to-end by alternating primary orthogonal joints and primary chord center-hinge joints, wherein said primary orthogonal joints have different geometry th

1. A deployable truss, comprising: at least two primary chords, said primary chords comprising a plurality of primary chordal members connected end-to-end by alternating primary orthogonal joints and primary chord center-hinge joints, wherein said primary orthogonal joints have different geometry than the primary chord center-hinge joints;at least one secondary chord, said secondary chord comprising a plurality of secondary chordal members connected end-to-end by alternating secondary orthogonal joints and secondary chord center hinge-joints, wherein said secondary chord hinge joints have different geometry than the secondary chord center-hinge joints; anda plurality of fixed-length diagonal members, each with a first end and a second end, the first end jointedly connected to a primary orthogonal joint, and the second end jointedly connected to a secondary orthogonal joint, wherein the primary orthogonal joints are not vertically or laterally aligned with the secondary orthogonal joints;a plurality of support struts extending between the primary orthogonal joints and the secondary chord center hinge-joints;wherein one or more of said support struts latch to the secondary chord center hinge joints when the truss is fully expanded; andwherein the primary chordal members fold inward in a plane at an angle to the folding planes of the secondary chords when the truss is retracted. 2. The truss of claim 1, wherein the primary chordal members folding angle is orthogonal. 3. The truss of claim 1, wherein the diagonals are connected to the primary orthogonal joints and secondary orthogonal joints with end fittings having offset hinge axes allowing the diagonals to nest parallel to each other when folded. 4. The truss of claim 1, comprising two secondary chords, so that the truss has a rectangular or square cross-section when the truss is fully expanded. 5. The truss of claim 4, further comprising a plurality of panels extending between the secondary chords. 6. The truss of claim 5, wherein the panels are solar panels, heat radiation panels, floor panels, wall panels, LCD panels, display panels, or radar panels, or combinations thereof. 7. The truss of claim 1, wherein each primary orthogonal joint comprises a single two- or three-axis fitting connected to the first end of a diagonal member. 8. The truss of claim 7, wherein the fitting comprises a clevis fitting. 9. The truss of claim 1, comprising one secondary chord, so that the truss has a triangular cross-section when the truss is fully expanded. 10. The truss of claim 9, wherein the primary chordal members fold inward in a plane at an angle to the folding planes of the diagonals when the truss is retracted. 11. The truss of claim 9, wherein the diagonals are connected to the respective primary orthogonal joints and secondary orthogonal joints with angled end fittings that permit the diagonals to fold at a selected angle. 12. The truss of claim 11, wherein the angled fittings comprise offset hinge axes that permit the diagonals to nest parallel to each other when the truss is retracted. 13. The truss of claim 1, wherein each primary orthogonal joint comprises a 3-axis fitting whereby adjacent primary chordal members are connected directly to the primary orthogonal joint. 14. The truss of claim 1, further comprising power actuators connected to one or more of said support struts. 15. A deployable truss, comprising: three primary chords, said primary chords comprising a plurality of primary chordal members connected end-to-end by alternating primary orthogonal joints and primary chord center-hinge joints, wherein said primary orthogonal joints have different geometry than the primary chord center-hinge joints;four secondary chords, said secondary chords comprising a plurality of secondary chordal members connected end-to-end by alternating secondary orthogonal joints and secondary chord center hinge-joints, wherein said secondary chord hinge joints have different geometry than the secondary chord center-hinge joints; anda plurality of fixed-length diagonal members, each with a first end and a second end, the first end jointedly connected to a primary orthogonal joint, and the second end jointedly connected to a secondary orthogonal joint, wherein the primary orthogonal joints are not vertically or laterally aligned with the secondary orthogonal joints;wherein said three primary chords and four secondary chords are arranged in a double row configuration, wherein the four secondary chords comprise two outside secondary chords and two center secondary chords, and the three primary chords comprise two outside primary chords and a center primary chord. 16. A deployable truss, comprising: three primary chords, said primary chords comprising a plurality of primary chordal members connected end-to-end by alternating primary orthogonal joints and primary chord center-hinge joints, wherein said primary orthogonal joints have different geometry than the primary chord center-hinge joints;four secondary chords, said secondary chords comprising a plurality of secondary chordal members connected end-to-end by alternating secondary orthogonal joints and secondary chord center hinge-joints, wherein said secondary chord hinge joints have different geometry than the secondary chord center-hinge joints; anda plurality of fixed-length diagonal members, each with a first end and a second end, the first end jointedly connected to a primary orthogonal joint, and the second end jointedly connected to a secondary orthogonal joint, wherein the primary orthogonal joints are not vertically or laterally aligned with the secondary orthogonal joints;wherein said three primary chords and four secondary chords are arranged in a double row configuration;further comprising a plurality of support struts extending between the primary orthogonal joints and the secondary chord center hinge-joints on the outside chords, and a plurality of center support struts extending between the primary orthogonal joints and the secondary chord center hinge-joints on the center chords. 17. The truss of claim 16, further comprising power actuators connected to one or more of said support struts and center support struts. 18. The truss of claim 16, wherein one or more of said support struts and center support struts latch to the corresponding secondary chord center hinge joints when the truss is fully expanded.