Lasinta Ari Nendra Wibawa (2019) Desain dan Analisis Tegangan Alat Pengangkat Roket Kapasitas 10 Ton Menggunakan Metode Elemen Hingga. Jurnal Energi dan Teknlogi Manufaktur (JETM), 02 (01). pp. 23-26. ISSN 2620-8741
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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. Kata
| Item Type: | Article |
|---|---|
| Uncontrolled Keywords: | aluminium 7075, autodesk inventor 2017, metode elemen hingga, alat pengangkat roket, analisis tegangan |
| Subjects: | Taksonomi LAPAN > Teknologi Penerbangan dan Antariksa > Penelitian, Pengembangan, Perekayasaan, dan Pemanfaatan > Teknologi Roket |
| Divisions: | LAPAN > Deputi Teknologi Penerbangan Dan Antariksa > Pusat Teknologi Roket > Balai Uji Teknologi Dan Pengamatan Antariksa Dan Atmosfer Garut |
| Depositing User: | Administrator Repository |
| Date Deposited: | 08 Jun 2021 08:40 |
| Last Modified: | 18 Jul 2022 08:20 |
| URI: | https://karya.brin.go.id/id/eprint/11645 |
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