A LOW SHOCK BALL-LOCK SEPARATION MECHANISM FOR SEPARATING UPPER STAGE AND SATELLITES FROM A SPACE LAUNCH VEHICLE

• 1. 用以将卫星从发射器或卫星分配器分离的连接/分离装置 [P] . 中国专利： CN110087997A . 2019-08-02
• 2. 一种低轨卫星组批发射星箭分离解锁模块和星箭分离的方法 [P] . 中国专利： CN112373734B . 2022.02.15
• 3. A LOW SHOCK BALL-LOCK SEPARATION MECHANISM FOR SEPARATING UPPER STAGE AND SATELLITES FROM A SPACE LAUNCH VEHICLE [P] . IN213933B . 2008-03-31

  机译： 用于从太空发射车上分离阶段和卫星的低冲击球锁分离机制

• 4. Shock-proof pyro mechanism for use in space applications, e.g. strap cutter used in launcher or satellite, includes low melting point metal that produces shock absorbing function when melted [P] . 法国专利： FR2801649A1 . 2001-06-01

  机译： 防震热释电机构，用于太空应用，例如用于发射器或卫星的带式切割机，包括低熔点金属，熔化后可产生减震功能

• 5. METHOD OF LAUNCHING MULTI-STAGE SPACE LAUNCH VEHICLE BY MEANS OF CARRIER-AIRCRAFT AND MULTI-STAGE SPACE LAUNCH VEHICLE FOR REALIZATION OF THIS METHOD [P] . 俄罗斯专利： RU2265559C1 . 2005-12-10

  机译： 通过航空器和多级空间发射车发射多级空间发射车辆的方法来实现该方法

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• 5. Monte Carlo simulation of stage separation dynamics of a multistage launch vehicle [J] . J. Roshanian, M. Talebi 应用数学和力学：英文版 . 2008,第011期
• 6. DEVELOPMENT STATUS OF LOW-SHOCK PAYLOAD SEPARATION MECHANISM FOR H-IIA LAUNCH VEHICLE [C] . Keita Terashima, Toru Kamita, Youichi Horie, 15th European space mechanisms and tribology symposium . 2013
• 7. Design and numerical simulation of a linear shaped charge separation mechanism for first stage separation of the Ares I launch vehicle. [D] . Chambers, Nicholas Roy. 2009
• 8. Adaptive Correlation Space Adjusted Open-Loop Tracking Approach for Vehicle Positioning with Global Navigation Satellite System in Urban Areas [O] . Hang Ruan, Jian Li, Lei Zhang, 2015
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