DESIGN AND ANALYSIS OF THERMO – VIBRATIONAL EFFECTS ON SPACE RE-ENTRY WEHICLE
Author(s):
S.L. PRADEEP KUMAR, C.SHAFANA, E.KATHIRAVAN, G.HARI HARAN, R.SANTHOSH KUMAR
Keywords:
Abstract
Re-entry vehicle is the part of space craft that is designed to return through earth is atmosphere. It is built to intense heating during high velocity flight through the atmosphere and to protect the crew and/or instrument until it bring them safety to earth. Aero thermodynamic analysis plays a critical role in designing a vehicle for hypersonic flight. Accurate information on the vehicle aerodynamic along the descent trajectory allows one to understand the capsule performance and therefore increase the payload and reduce the heat shield thickness on the vehicle. one of the main concerns of the aerodynamics of planetary entry is the heating rate and damage that this may cause to the vehicle at hypersonic flight speed during the reentry large fraction of the kinetic energy will be converted into heat that effect the vehicle. In this project we do shock wave, thermal and structural analysis of re-entry vehicle by using CFD software and by comparing the analysis results with the result of aerogel material and we conclude the application of aerogel to withstand the aerodynamic heating for future heat ablative materials in re-entry vehicle.
Article Details
Unique Paper ID: 148307

Publication Volume & Issue: Volume 6, Issue 1

Page(s): 362 - 368
Article Preview & Download




Publish book

Go To Issue



Call For Paper

Volume 6 Issue 2

Last Date 25 July 2019


About Us

IJIRT.org enables door in research by providing high quality research articles in open access market.

Send us any query related to your research on editor@ijirt.org

Social Media

Google Verified Reviews

Contact Details

Telephone:8200 61 5067
Email: editor@ijirt.org
Website: ijirt.org

Policies