Deployable antenna frame

The present invention relates to employable support structures for space applications, such as deployable reflector antennas. A multi-faceted deployable antenna frame is proposed, comprising a six-bar linkage structure in a lateral facet of the antenna frame (1), the six-bar linkage structure (100) being convertible from a folded state into a deployed state and having two first bars (3) and four second bars (5), each bar being coupled to two others by a hinge (4 or 20) to form a closed loop, wherein in the deployed state, the six-bar linkage structure (100) has a quadrilateral shape. The antenna frame further comprises a deployment means for deploying the antenna frame (1) by moving the six-bar linkage structures (100) from the folded state into the deployed state, the deployment means comprising: a flexible, elongated member (14) of a substantially inextensible material; a first guiding means (13) provided at an end portion of one of the first bars (3) and coupled to the elongated member (14); a storage means (16) provided at the first bar (3) that comprises the first guiding means (13) for storing a part of the elongated member (14); a driving means that is coupled to the elongated member (14) to pull the elongated member (14) to the storing means (13) when deploying the antenna frame (1); and a second guiding means (21) between two adjacent second bars (5), the elongated member (14) being coupled to the second guiding means (21). A first end of the elongated member (14) is attached to the storing means (16) and a second end of the elongated member (14) is coupled to another first bar (3), and wherein the elongated member (14) is extending between said first end and said second end along a plurality of second bars (5).