Multi-satellite collision-free release stacking mode and release method

The invention discloses a multi-satellite collision-free release stacking mode and release method, which comprises a plurality of layers of stacked single satellites, each layer comprises four release units, the four release units sequentially rotate by 90 degrees and are attached to one another, each release unit comprises two single satellites, namely a normal position satellite and a reverse position satellite, and the single satellites are cuboid-shaped. According to the multi-satellite collision-free release stacking mode and the multi-satellite collision-free release method, the mass of a distributor can be reduced or even eliminated, the structural rigidity and strength needed in the launching period are not damaged, and the multiple satellites are completely dispersed at a time under the condition of the specific initial angular velocity. 本发明公开了一种多卫星无碰撞释放的堆叠方式及释放方法，包括若干层堆叠的单颗卫星，每一层包括四个释放单元，四个释放单元依次旋转90°并相互贴合，每一个释放单元包括正位卫星和反位卫星两个单颗卫星，单颗卫星为长方体形。本发明采用上述结构的一种多卫星无碰撞释放的堆叠方式及释放方法，能够减少或甚至消除分配器质量，而不损及发射期间所需的结构