Estimation of Separation Shock of the Marman Clamp System by Using a Simple Band-Mass Model

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概要

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• To prevent satellite failure during inter stage separation, the magnitude of separation shock must be estimated. The Marman Clamp System is a separation joint often used to mount satellites on a launch vehicle. This paper proposes a method of estimating separation shock for the Marman Clamp System. First, experimental results are discussed and the dominant parameters of separation shock are identified for the system. Next, a simple band-mass model is proposed to estimate the system’s separation shock. The differences between the model and experimental results are discussed. Radial and axial, but not tangential, separation shocks were estimated well by this method.

• 社団法人 日本航空宇宙学会の論文
• 2002-05-04

著者

• ONODA Junjiro

  The Institute of Space and Astronautical Science

• Takeuchi Shinsuke

  The Institute Of Space And Astronautical Science

関連論文

• Semi-Active Vibration Suppression of Beam Structures Based on Energy-Recycling Method
• Estimation of Separation Shock of the Marman Clamp System by Using a Simple Band-Mass Model

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