DEVICE FOR OVERCOMING THE PROBLEM OF CREW SAFETY DURING A SPACECRAFT LAUNCH AND IMPROVE THE JOINTS CONNECTING THE SEGMENTS OF THE SOLID ROCKET BOOSTER

• 1. 一种飞行器级间连接段与助推器前封头一体化结构 [P] . 中国专利： CN112412659B . 2021.12.10
• 2. 一种飞行器级间连接段与助推器前封头一体化构型 [P] . 中国专利： CN112412659A . 2021-02-26
• 3. Device for overcoming the problem of crew safety during a spacecraft launch and improve the joints connecting the segments of the solid rocket booster [P] . 美国专利： US5108049A . 1992-04-28

  机译： 用于克服航天器发射期间人员安全问题并改善连接固体火箭助推器各部分的接头的装置

• 4. DEVICE FOR OVERCOMING THE PROBLEM OF CREW SAFETY DURING A SPACECRAFT LAUNCH AND INPROVE THE JOINTS CONNECTING THE SEGMENTS OF THE SOLID ROCKET BOOSTER [P] . 欧洲知识产权局专利： EP0303628B1 . 1991-04-03

  机译： 克服航天飞机发射过程中机组安全问题并改善连接固体火箭助推器段的接头的装置

• 5. DEVICE FOR OVERCOMING THE PROBLEM OF CREW SAFETY DURING A SPACECRAFT LAUNCH AND INPROVE THE JOINTS CONNECTING THE SEGMENTS OF THE SOLID ROCKET BOOSTER [P] . 欧洲知识产权局专利： EP0303628A1 . 1989-02-22

  机译： 克服航天飞机发射过程中机组安全问题并改善连接固体火箭助推器段的接头的装置

• 1. Solid Rocket Motors for Launch Escape Tower Provide Safety to Astronauts [J] . Zong He 中国航天（英文版） . 2012,第003期
• 2. A Position and Orientation Compensation Mechanism for Automatic Docking Device of Launch Rocket [J] . Zhou Cheng, Yu Cungui 南京航空航天大学学报（英文版） . 2018,第006期
• 3. A Position and Orientation Compensation Mechanism for Automatic Docking Device of Launch Rocket [J] . Zhou Cheng, Yu Cungui 南京航空航天大学学报（英文版） . 2018,第006期
• 4. ZTE Solidifies 3G Strategy with the Launch of a Comprehensive Array of 3G Devices [J] . 无 中兴通讯技术：英文版 . 2009,第002期
• 5. 3 m Twin-Segment Solid Rocket Engine Tested Successfully [J] . YAO Tianyu 中国航天（英文版） . 2016,第003期
• 6. Reliability and crew safety assessment for a solid rocket booster/J-2S launcher [C] . Fragola J., Baum J.D., Sauvageau D., Reliability and Maintainability Symposium, 2006. RAMS '06. Annual . 2006
• 7. A supportability simulation for the forward and aft integrated electronics assemblies on the Space Transportation System Solid Rocket Booster. [D] . Cassibry, Phillip J. 2005
• 8. Investigation of the THOR Anthropomorphic Test Device for Predicting Occupant Injuries during Spacecraft Launch Aborts and Landing [O] . Jeffrey T. Somers, Nathaniel Newby, Charles Lawrence, 2014
• 9. FE Analysis of Contact Pressure Prediction on O-Rings Used in Solid Rocket Booster Segment Joints [O] . V. Sivakumar, Amrita Vishwa, Amrita Nagar, 2013

• 1. 苗木捆扎机捆扎接头连接装置的设计 [C] . Cui teng jiao ,崔腾娇 . 中国农业工程学会2013年学术年会 . 2013
• 2. 基于积分球的发射率测量装置及纯铜在热氧化过程中的发射率研究 [A] . 张会燕 . 2019