Author(s)

Bin Yu^1,2*, TianJu Ma², Yun Zhang², Cheng Huang¹, SenDong Gu², HaiYan Li², LinFeng Chen²

Affiliation(s)

¹Light Alloy Research Institute, Central South University, Changsha 410000, Hunan, China.

²Aerospace Pressure Vessel Division, Lanzhou Institute of Physics, Lanzhou 730000, Gansu, China.

Corresponding Author

Bin Yu

ABSTRACT

This paper systematically reviews global progress in composite overwrapped pressure vessels (COPVs) for space applications and projects their trajectory, synthesizing key advances from the United States, Europe and leading Asian nations in structural and reliability design, stress-fracture and low-cycle-fatigue life prediction, material selection, forming, qualification and non-destructive testing, including high-strength fibers, ultra-thin metallic liners, inheritable design principles and validated failure models, and summarizing representative work by principal Chinese institutes and universities; on this basis it proposes future Chinese directions-high-strength fiber optimization, advanced liner alloys, burst-factor and performance-factor tuning, next-generation NDT, upstream pre-research and Standardization-to underpin independent R&D and technological upgrading of high-performance aerospace COPVs.

KEYWORDS

Aerospace propulsion systems; Composite pressure vessels; Metal liners; Fiber-reinforced composites; Reliability; Stress fracture life

CITE THIS PAPER

Bin Yu, TianJu Ma, Yun Zhang, Cheng Huang, SenDong Gu, HaiYan Li, LinFeng Chen. Composite over-wrapped pressure vessel technology for spacecraft propulsion systems. Journal of Manufacturing Science and Mechanical Engineering. 2025, 3(1): 53-67. DOI: https://doi.org/10.61784/msme3020.

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