Modeling and simulation of separation process in flotation system

2009 ◽  
Vol 15 (2) ◽  
pp. 196-201 ◽  
Author(s):  
Byoung-Uk Cho ◽  
Jeong-Yong Ryu ◽  
Bong-Keun Song
2011 ◽  
Vol 141 ◽  
pp. 359-363 ◽  
Author(s):  
Jun Lan Li ◽  
Shao Ze Yan ◽  
Xue Feng Tan

The clamp band system is a typical locked and separated device of the launch vehicle (LV) / the spacecraft (SC), and its release-separation process is one of the important factors that affect the LV/SC separation movement. A nonlinear spring-damper model was employed to describe the contact-impact behavior between the V-segment of the clamp band and the LV/SC interface, and lumped mass method was used to depict the clamp band. By using ADAMS, a dynamic model of the clamp band system was established. The simulation results show that the impulse of the explosive bolts and the stiffness of lateral-restraining springs have significant effects on the clamp band dynamic envelope. The shock of the satellite-vehicle separation is very vulnerable to the clamp band pretension and the friction coefficient between the V-segment and the LV/SC interface.


2016 ◽  
Vol 9 (1) ◽  
pp. 72-78 ◽  
Author(s):  
Kambiz Tahvildari ◽  
Seyed Mohammad Reza Razavi ◽  
Hamed Tavakoli ◽  
Ashkan Mashayekhi ◽  
Reza Golmohammadzadeh

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