摘要
                
                    为了梳理和分析星舰-超重体系与开发的模式,及其相比以往航天运输体系的变革,本文首先回顾星舰-超重的宏观演化与微观验证历程,而后评估基于星舰-超重的太空新物流体系优势与挑战,最后探讨资本驱动下航天运输系统价值网升维与开发范式变革的内在逻辑。研究发现:星舰-超重的开发理念是“创新引领,市场运作;宏观演化,微观验证”,本质是资本内在增值需求推动新技术、新平台的快速集成和应用。
                
                The evolution and intelligent technology prospect of the starship-superheavy system is analyzed in comparison with previous space transportation systems.First,the processes of macro-evolution and micro-verification for the starship-superheavy system are reviewed.Then,the advantages and challenges of the new space logistics system are assessed based on the starship-superheavy system.Finally,the internal logic of the evolution and intelligent technology prospect is investigated based on the capital-driven space transportation system.The results show that the development concept of starship-superheavy is“innovation-driven,market operation;macro-evolution,microverification”.The essence is that the internal needs of capital gain promote the rapid integration and application of new technologies and new platforms.
    
    
                作者
                    吴佳林
                    盛英华
                    程川
                    张众
                WU Jialin;SHENG Yinghua;CHENG Chuan;ZHANG Zhong(Shanghai Academy of Spaceflight Technology,Shanghai 201109,China;Shanghai Aerospace System Engineering Institute,Shanghai 201109,China)
     
    
    
                出处
                
                    《上海航天(中英文)》
                        
                                CSCD
                        
                    
                        2024年第3期87-94,共8页
                    
                
                    Aerospace Shanghai(Chinese&English)
     
    
                关键词
                    星舰-超重
                    太空物流体系
                    开发范式变革
                    水平减速与垂直起降
                
                        starship-superheavy
                        space logistics system
                        evolution and intelligent
                        horizontal deceleration and vertical take-off/landing
                
     
    
    
                作者简介
吴佳林(1981-),男,研究员,主要研究方向为运载火箭总体设计。