PERANCANGAN DAN PEMBUATAN LAUNCHER UNTUK PESAWAT UAV SUA SERIES

PUTRA SILAWAN, ANGGIT (2018) PERANCANGAN DAN PEMBUATAN LAUNCHER UNTUK PESAWAT UAV SUA SERIES. Skripsi thesis, Institut Teknologi Dirgantara Adisutjipto.

[img] Text (ABSTRAK)
10050083_ABSTRAK.pdf

Download (197kB)
[img] Text (BAB I)
10050083_BAB I.pdf

Download (123kB)
[img] Text (DAFTAR PUSTAKA)
10050083_DAFTAR PUSTAKA.pdf

Download (104kB)
[img] Text (FULL SKRIPSI)
10050083.pdf
Restricted to Repository staff only

Download (2MB)

Abstract

On this occasion the author raises the research topic in the Design and Manufacture of Launchers for SUA Series UAV Aircraft, the production process is based on the calculation of the potential energy of the spring and the force produced by the spring so that the author can determine the length of the real launcher to be produced. Preparation of tools and materials in the production process is based on the force required by the SUA series UAV aircraft in order to take off. The launcher manufacturing process begins by determining the type of UAV aircraft to be launched, the spring to be used and the purchase of materials for making the launcher. Based on the calculation and experimental data obtained, the spring constant value is 380.4 N / m, pulled 1.7m then released and is able to push the aircraft with an initial aircraft speed produced by the launcher of 15 m / s.

Item Type: Thesis (Skripsi)
Subjects: T Technology > T Technology (General)
Divisions: Institut Teknologi Dirgantara Adisujtipto > Teknik Dirgantara
Depositing User: Mr ANGGIT PUTRA SILAWAN
Date Deposited: 23 Jul 2024 06:45
Last Modified: 23 Jul 2024 06:45
URI: http://eprints.stta.ac.id/id/eprint/2336

Actions (login required)

View Item View Item

Downloads

Downloads per month over past year