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Liu, Y.Q. (1993) Preliminary Study on Snap-Ring Connection Structure of Solid Rocket Motor Nozzle and Case. Journal of Solid Rocket Technology, 1, 1-5. (In Chinese)
https://kns.cnki.net/kcms2/article/abstract?v=QP2K49WHhimGshRjuN0kPA9tC6JFwx8TlP18y7jVFY0sPThvz-svwJ0GWca0vhybXpn9aoSYCmTFn24f0RxuB86LBFkxrxKSTIxPCgNyY8638Wg5EBjCvvzqWPjtQ88suKnAIodfMvSdP1Fu8u8yODHgmORetR1M&uniplatform=NZKPT

has been cited by the following article:

• TITLE: Research on Universal Clamping Technology for Automatic Assembly of Small Solid Rockets

  AUTHORS: Xudong Wang, Jinyan Liao, Lei Huang, Huiqiang Wang, Zihao Chen, Dawei Zhang, Zhen Xu

  KEYWORDS: Clapping, Solid Small Rockets

  JOURNAL NAME: World Journal of Engineering and Technology, Vol.14 No.3, July 14, 2026

  ABSTRACT: Based on an analysis of clamping methods for the automatic assembly of small solid rockets, clamping force calculation, simulation, and experimental verification were carried out for different clamping solutions. The results show that when using a three-jaw chuck fitted with a 0.5 mm thick graphite rubber pad between the chuck jaws and the rocket shell, a clamping pressure of 0.5 MPa can prevent slippage even under the maximum torque load of 390 N∙m. The resulting deformation has no adverse impact on product quality and assembly performance. Considering the profile characteristics of the clamping surface of small solid rockets and economic efficiency, a universal clamping tooling was designed. This work lays a foundation for the automatic assembly of small solid rockets.