1. 毕业设计（论文）的内容和要求
有效载荷分离是整个运载火箭发射任务的最后一个环节，也是一个短暂却十分关键的过程，直接影响发射任务的成败。
完成一次有效载荷发射任务主要包括以下四个分离过程：助推器分离、火箭级间分离、整流罩分离与有效载荷分离，而有效载荷分离直接决定了卫星能否准确进入预定轨道。
有效载荷分离装置结构尺寸对分离过程的可靠性影响较大。
2. 参考文献
[1] M. Tayefi, M. Ebrahimi. Design and Analysis of Separation Systems Based on an OptimizationApproach .AIAA. 2009.[2] B. Morse, A. Wittmann. Shear Load Carrying V-clamp for Spaceraft Application. Patent No. 4715565, 1987[3] P.R. Klarer, M.R . Vaughn, J.F. Gilbride, R.S. Baty, and J. L. Adams, Design for an Internal Circular Compression Band Restraint Device, SAND Report,2002-2744[4] Peffer A. Development and transition of low-shock spacecraft release devices for small satellites[C]. 14th Annual/USU Conference on Small Satellites, 2001.[5] Dowen D, Christiansen S. Development of a reusable, low-shock clamp band separation system for small spacecraft release applications[C]. EuropeanSpace Mechanisms Tribology Symposium, 2001: 191-198.
