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Lasinta Ari Nendra Wibawa
Badan Riset dan Inovasi Nasional (BRIN)
Aerospace Engineering Automotive Engineering Chemical Engineering, Chemistry & Bioengineering Civil Engineering, Building, Construction & Architecture Computer Science & IT Control & Systems Engineering Decision Sciences, Operations Research & Management Education Electrical & Electronics Engineering Energy Engineering Industrial & Manufacturing Engineering Materials Science & Nanotechnology Mechanical Engineering Physics Transportation

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Journal : Jurnal Energi dan Teknologi Manufaktur (JETM)

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Desain dan Analisis Tegangan Alat Pengangkat Roket Kapasitas 10 Ton Menggunakan Metode Elemen Hingga Lasinta Ari Nendra Wibawa
Jurnal Energi dan Teknologi Manufaktur Vol 2 No 01 (2019)
Publisher : Polinema Press, Politeknik Negeri Malang

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.33795/jetm.v2i01.31

Abstract

This study examines the design and stress analysis of a 10 ton capacity rocket lifting device using the finite element method. The material used is Aluminum alloy 7075. Finite element analysis is done numerically by using Autodesk Inventor Professional 2017. software The simulation results show that the structure of the rocket lift has Von Mises stress, deformation, mass, and safety factors of 46.34 MPa, 0.7947 mm, 186.75 kg, and 3.13.
Co-Authors Abdilah Hasan Hasan Adi Farmasiantoro Farmasiantoro Alit Daryana Asep Diana Diyat Muhdiyat Muhdiyat Dwi Aries Himawanto Dwi Aries Himawanto Gatot Suharto Abdul Fatah Handriyana Handriyana Iyus Rusyana Rusyana Jihad, Bagus H. Kukuh Yudistiro Kuncoro Diharjo Kuncoro Diharjo Parid Saparudin Rahadyan Lingga Laksita Toris Sobirin Tuswan Tuswan Unggul Satrio Yudhotomo Unggul Satrio Yudhotomo Wan Dedy Fitrah Indrayana Wijang Wisnu Raharjo Yopiek Kristiyana Kristiyana Yudi Haryanto Yudi Prastiyono