TY - JOUR
T1 - 新一代载人飞船逃逸系统设计与关键技术研究
AU - Tian, Lin
AU - Wu, Xinfeng
AU - Wang, Pengcheng
AU - Jing, Xuzhen
AU - Zhang, Haowei
AU - Hao, Ping
AU - Xu, Ming
AU - Gong, Chunlin
N1 - Publisher Copyright:
© 2023 China Spaceflight Society. All rights reserved.
PY - 2023/9
Y1 - 2023/9
N2 - The safety of astronauts is of utmost importance in any manned space mission. That' s why the launch abort system (LAS) of China' s next-generation manned spacecraft has been designed with meticulous attention to detail. From entering the cabin to entering the orbit, every step has been analyzed using the MBSE method to ensure the system meets the highest safety standards. This system is specifically aimed at manned lunar exploration and low-Earth-orbit space station missions, making it a crucial component of any manned space program. The launch abort mode and system design have been studied and determined, with special research conducted in various aspects such as trajectory and control, structure and separation, aerodynamics, power, and information. The identified technical difficulties have been overcome with proposed solutions, and the development of key technologies has been summarized. LAS will undergo full assessment and verification in subsequent development to ensure stable and reliable operation during formal flight missions. With this new launch abort system, the safety of manned spaceflight missions can be further enhanced and improved.
AB - The safety of astronauts is of utmost importance in any manned space mission. That' s why the launch abort system (LAS) of China' s next-generation manned spacecraft has been designed with meticulous attention to detail. From entering the cabin to entering the orbit, every step has been analyzed using the MBSE method to ensure the system meets the highest safety standards. This system is specifically aimed at manned lunar exploration and low-Earth-orbit space station missions, making it a crucial component of any manned space program. The launch abort mode and system design have been studied and determined, with special research conducted in various aspects such as trajectory and control, structure and separation, aerodynamics, power, and information. The identified technical difficulties have been overcome with proposed solutions, and the development of key technologies has been summarized. LAS will undergo full assessment and verification in subsequent development to ensure stable and reliable operation during formal flight missions. With this new launch abort system, the safety of manned spaceflight missions can be further enhanced and improved.
KW - Design of launch abort system
KW - Low-Earth-orbit space station
KW - Manned lunar exploration
KW - Next-generation manned spacecraft
UR - http://www.scopus.com/inward/record.url?scp=85176228675&partnerID=8YFLogxK
U2 - 10.3873/j.issn.1000-1328.2023.09.008
DO - 10.3873/j.issn.1000-1328.2023.09.008
M3 - 文章
AN - SCOPUS:85176228675
SN - 1000-1328
VL - 44
SP - 1350
EP - 1359
JO - Yuhang Xuebao/Journal of Astronautics
JF - Yuhang Xuebao/Journal of Astronautics
IS - 9
ER -