This paper presents a design theory and dynamic mechanical characterizations of the composite tape-spring hinge made by two parallel single tape springs. First, the theoretical models of moment-rotation angle on anisotropy tape springs with antisymmetric laminates are proposed. Second, the relationships of moment-rotation angle for tape-spring hinges with different sizes are simulated and analyzed by means of the finite element method (FEM), which is in good agreement with the results from theoretical predictions. Finally, the dynamic vibration analysis for deployable composite tube hinges with different dampings is done during the process of deployment. Composite tape-spring hinge, deployable, dynamic, damping PACS: 46.40.Ff, 46.70.De, 81.05.QkThe composite tape hinge is a self-deployable and selfdrivable structure, which has wide engineering applications in spacecraft structures due to its high specific strength, high specific stiffness, zero expansion and high damping ratio.Most studies about mechanical behaviors of tape spring are concentrated on the isotropic thin shell structure. Mansfiel [1] described the relationships between bending moment, torque moment, longitudinal and twisting curvatures for the isotropic initially curved strips. Seffen et al. [2,3] and Walker et al.[4] determined the moment-rotation angle relationships and the maximum moments of isotropic tape spring for opposite-sense and equal-sense bending theoretically. Walker et al. [5,6] performed the pure bending experiments of the single isotropic tape spring for opposite sense and equal sense with different sizes. For the composite tape hinge, Galletly et al. studied the cross-sectional shape and equilibrium point for the bistable composite tape hinge by the beam model [7] and the shell model [8]. Soykasap [9] studied the deployable behaviors of the hardened-steel tape-spring hinge using a theoretical model and non-linear finite element methods. Yee et al.[10] studied the bending behaviors for the one-ply and two-ply laminated tape spring made by carbon fiber reinforced plastic (CFRP). Lei et al. [11] investigated the deployment properties of carbon/epoxy and glass/epoxy thin cylindrical shell by means of bending test and theoretical analysis. On the other hand, Yee et al. [12] and Soykasap [13] studied the moment-rotation angle relationships and strain distribution of the composite tape-spring hinge made by three parallel single tape springs using FEM; Hoffait et al. [14] studied the rotation angle, bending moment and energy of the isotropic three-tape-spring hinge during the deployment.In this paper, the deployment behaviors of the anisotropy tape-spring hinges are investigated by means of a theoretical model. And the dynamic vibration characterizations for the composite tape-spring hinges with different dampings are studied during the process of deployment.