Erectable concepts for large space system technology

Abstract

Design features of components for space erectable/deployable concepts are described along with the neutral buoyancy testing with the shuttle remote manipulator system. The basic structural configuration is a double folding cubic module. It is 3 meters by 3 meters in crosssection by 6 meters long. The first folding operation results in a 3 meter by 6 meter planar configuration. The second folding operation results in a 9 meter linear configuration. Folding (deployment) is achieved by single and double pivoting joints and telescoping diagonal members. Deployment and retraction is accomplished by an external force. Two joining devices, the module to module coupler and the automatic coupler, were designed and fabricated for test. The module to module coupler features angular and axial locking compliances of 10 deg and 2.5 mm, respectively. It also has a linear zero free play stiffness characteristic.