In the future， high-precision loads impose stringent requirements on the dimensional stability of spacecraft structures.The sandwich structure of carbon fiber-reinforced polymer （CFRP） honeycomb is a new lightweight structural design with excellent thermal dimensional stability，capable of meeting the design requirements for load-bearing structures under such conditions.This paper reviews the current development status of CFRP honeycomb manufacturing methods.Based on the manufacturing processes and corresponding technology methods that influence the dimensional stability of CFRP honeycomb structures，the manufacturing methods are categorized into two main types：multi-step forming methods and integral forming methods.The technical advantages and disadvantages of various manufacturing methods are analyzed，and the technical challenges of new manufacturing methods are discussed.Finally，the future development direction of manufacturing technology for dimensionally stable CFRP honeycombs is explored.