C. Li, Z. Zhang, Q. Yang and P. Li, Experiments on the geometrically nonlinear vibration of thin-walled cylindrical shells with points supported boundary condition, Journal of Sound and Vibration, Vol. 473, 115226, 2020.
 G. Li, Z. Nie, Y. Zeng, J. Pan and Z. Guan, New Simplified Dynamic Modeling Method of Bolted Flange Joints of Launch Vehicle, Journal of Vibration and Acoustics, Vol. 142, No. 2, 2020.
 Z.-Y. Qin, S.-Z. Yan and F.-L. Chu, Dynamic characteristics of launch vehicle and spacecraft connected by clamp band, Journal of Sound and Vibration, Vol. 330, pp. 2161-2173, 2011.
 Z. Y. Qin, S. Z. Yan and F. L. Chu, Dynamic analysis of clamp band joint system subjected to axial vibration, Journal of sound and vibration, Vol. 329, pp. 4486-4500, 2010.
 A. Davar, S. S. Mousavi and R. Azarafza, Reliability Analysis of Bearing Load Capacity of V-Clamp Band Under Parameters’ Uncertainty, Journal of Mechanical Engineering, Vol. 51, N0. 3, pp. 41-49, 2019. (in Persion)
 Z. Y. Qin, S. Z. Yan and F. L. Chu, Influence of clamp band joint on dynamic behavior of launching system in ascent flight, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 228, pp. 97-114, 2014.
 Z. Y. Qin, S. Z. Yan and F. L. Chu, Analytical modeling of clamp band joint under external bending moment, Aerospace Science and Technology, Vol. 25, pp. 45-55, 2013.
 Z. Y. Qin, S. Z. Yan and F. L. Chu, Dynamic analysis of slender launching system connected by clamp band joint using harmonic balance method, in Journal of Physics: Conference Series, Vol. 448, 2013.
 H. Li, M. Zhu, Z. Xu, Z. Wang and B. Wen, The influence on modal parameters of thin cylindrical shell under bolt looseness boundary, Shock and Vibration, Vol. 2016, pp. 1-15, 2016.
 Q. Tang, C. Li, H. She and B. Wen, Modeling and dynamic analysis of bolted joined cylindrical shell, Nonlinear Dynamics, Vol. 93, pp. 1953-1975, 2018.
 Q. Tang, C. Li, H. She and B. Wen, Vibration analysis of bolted joined cylindrical-cylindrical shell structure under general connection condition, Applied Acoustics, Vol. 140, pp. 236-247, 2018.
 F. Wang, J. Li, Y.-q. Li and Z. Luo, The investigation of vibration characteristics on the bolted disk--drum joints structure, Advances in Mechanical Engineering, Vol. 11, 1687814019831477, 2019.
 Y. Liu, J. Wang and L. Chen, Dynamic Characteristics of the Flange Joint with a Snap in Aero-Engine, International Journal of Acoustics and Vibration, Vol. 23, pp. 168-174, 2018.
 M. M. Ataei, H. Salarieh, H. NejatPishkenari and H. Jalili, Boundary control design for vibration suppression and attitude control of flexible satellites with multi-section appendages, Acta Astronautica, Vol. 173, pp. 22-30, 2020.
 T. Kitamura, K. Yoshida, H. Seko, Q. Shi, Analysis of shock response for satellite separation, Proceeding of ISME2012, USD2012, pp. 2091-2102, 2012.
 X. Wang, W. Liu, X. Li and Y. Sun, The Shock Response Prediction of Spacecraft Structure Based on Hybrid FE-SEA Method, Applied Sciences, Vol, 11, pp. 1-17, 2021.
 D. Cui, S. Yan, J. Li, Z. Qin and X. Guo, Dynamic analysis of satellite separation considering the flexibility of interface rings, Proc IMechE Part G: J Aerospace Engineering, Vol. 0, pp. 1–17.
 A. Davar, R. Azarafza, and S. S. Mousavi, Uncertainty analysis and reliability estimation of clamp band joints, Materials Science and Technology, Vol. 36, pp. 1487-1502, 2020.
 J. Odeon, Mechanics of elastic structures, New York: McGraw-Hill, Inc., 1976, pp. 83-130.
 C. Zheng, G. Ruo-fei and S. Lei, LM-3A series launch vechicle user's manual, China Academy of Launch Vehicle Technology, 2011.
 N. A. S. A. GD-ED, "2214, Marman Clamp System Design Guidelines, 2000.