Structural Analysis of Satellite Launch Vehicle for Aerospace Applications

dc.contributor.author	M Faizan shabbir Ahmed naveed M Hamza daud Muhammad Waqas, supervised by Dr Niaz Bahadur Khan
dc.date.accessioned	2022-06-28T05:31:10Z
dc.date.available	2022-06-28T05:31:10Z
dc.date.issued	2022
dc.identifier.uri	http://10.250.8.41:8080/xmlui/handle/123456789/29759
dc.description.abstract	Pakistan does not have its own satellite launch vehicle yet, so we are helping our industry to develop one. Our project “Structural Analysis of Satellite Launch Vehicle for Aerospace Applications” includes the aerodynamic analysis of the exterior of the rocket and the structural analysis of the body to find out that the 3D model of the rocket made holds valid for the applied loads that the rocket will undergo during its flight. The next step will be the development of the model for tunnel testing and then making an actual rocket but that also includes other systems such as control system, propulsion system which are beyond our scope this project.	en_US
dc.language.iso	en	en_US
dc.publisher	SMME	en_US
dc.subject	Satellite, Aerospace	en_US
dc.title	Structural Analysis of Satellite Launch Vehicle for Aerospace Applications	en_US
dc.type	Thesis	en_US