Linear Analysis of a Cryo Propellant Tank |
Author(s): |
| Anu Retnakar , AHALIA SCHOOL OF ENGINEERING & TECHNOLOGY; Ajin A. S., AHALIA SCHOOL OF ENGINEERING & TECHNOLOGY |
Keywords: |
| Propellant, Linear Analysis, Yield Strength, Axisymmetric Modeling, Plane 82 |
Abstract |
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There are many stages for satellite launch vehicles. Among them cryo stages use fuels or oxidizers at low temperatures. Propellants are stored in propellant tanks. Tank will be subjected to pressure loads. A cryo propellant tank having liquid hydrogen was modelled axisymmetrically using ANSYS. Linear analysis is performed on it. From the results it was obtained that the equivalent von Mises stress exceeded ultimate tensile strength. |
Other Details |
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Paper ID: IJSRDV7I40703 Published in: Volume : 7, Issue : 4 Publication Date: 01/07/2019 Page(s): 588-591 |
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