1.School of Mechanical Engineering,Shanghai Jiaotong University,Shanghai 200240,China 2.Shanghai Academy of Spaceflight Technology,Shanghai 201109,China 3.Aerospace System Engineering Shanghai,Shanghai 201109,China 4.Beijing Institute of Tracking and Telecommunication Technology,Beijing 100190,China
LUO M, CHEN S Q, LI D P,et al. Characteristics of starship propulsion system and numerical simulation of propellant flow during reentry[J]. Journal of Nanjing University of Aeronautics & Astronautics,2021,53(S):9⁃16 (in Chinese).
ZHANG Y J, ZUO G, XU Y Z, at et. Numerical simulation on aerodynamic characteristics of new type control surface of Starship[J]. Acta Aeronautica et Astronautica et Astronautica Sinica, 2021, 42(2): 624058 (in Chinese).