Modeling and simulation of a Carbon13C Separation Process by low temperature Distilation

Author(s):  
Sas Diana Monica ◽  
Kovendi Zoltan ◽  
Coroiu Laura ◽  
Gergely Eugen Ioan ◽  
Husi Geza
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.


2009 ◽  
Vol 15 (2) ◽  
pp. 196-201 ◽  
Author(s):  
Byoung-Uk Cho ◽  
Jeong-Yong Ryu ◽  
Bong-Keun Song

2017 ◽  
Vol 114 ◽  
pp. 1488-1494
Author(s):  
Benjamin Decardi-Nelson ◽  
Ananda Akachuku ◽  
Priscilla Osei ◽  
Wayuta Srisang ◽  
Fatemeh Pouryousefi ◽  
...  

Energies ◽  
2018 ◽  
Vol 11 (6) ◽  
pp. 1591 ◽  
Author(s):  
Alessandro Sbrana ◽  
Paola Marianelli ◽  
Giuseppe Pasquini ◽  
Paolo Costantini ◽  
Francesco Palmieri ◽  
...  

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