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All Journal Jurnal Ergonomi Indonesia (The Indonesian Journal of Ergonomic) Jurnal Penelitian Fisika dan Aplikasinya (JPFA) Jurnal Teknosains Jurnal Dunia Kesmas Jurnal Teori dan Aplikasi Fisika Jurnal Migasian Akamigas Balongan Indramayu Indonesian Journal of Innovation and Applied Sciences (IJIAS) Newton-Maxwell Journal of Physics Jurnal Migasian Jurnal Pengabdian Masyarakat dan Riset Pendidikan
Qonitatul Hidayah
Department Of Physics - Universitas Ahmad Dahlan
Humanities Astronomy Biochemistry, Genetics & Molecular Biology Chemical Engineering, Chemistry & Bioengineering Chemistry Civil Engineering, Building, Construction & Architecture Decision Sciences, Operations Research & Management Earth & Planetary Sciences Economics, Econometrics & Finance Education Electrical & Electronics Engineering Energy Engineering Environmental Science Health Professions Industrial & Manufacturing Engineering Languange, Linguistic, Communication & Media Materials Science & Nanotechnology Mathematics Mechanical Engineering Physics Public Health Social Sciences Other

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Analisis Uji Peluncuran Roket Air Berbasis Carbon Fiber Menggunakan Sistem Telemetri Qonitatul Hidayah; Umi Salamah; Margi Sasono
Jurnal Teori dan Aplikasi Fisika Vol. 10 No. 1 (2022): Jurnal Teori dan Aplikasi Fisika
Publisher : Department of Physics, Faculty of Mathematics and Natural Sciences, University of Lampung

Show Abstract | Download Original | Original Source | Check in Google Scholar | DOI: 10.23960/jtaf.v10i1.288

Abstract

Rocket technology with water propellant is becoming more popular and as an alternative to be applied to education and recreation, such as industry and the military. The use of water rockets as an easy, safe, and inexpensive means of measuring physical parameters at heights above the earth's surface is being intensively carried out. One alternative solution is aerodynamic water rocket technology equipped with a telemetry system. The rocket used for the test launch is made from untested carbon fiber. Flight test settings by filling 1/3 of the tube volume with water and a pressure of 200 psi. The results of the water rocket launch show a maximum height of 265 feet or 80.77 m. Changes in acceleration on the x-axis, y-axis, and z-axis indicate the normal motion of the flying rocket. Analysis of stability and control of the rocket is seen in the measurement of the tilt angle of roll, pitch, and yaw. When the rocket moves or tilts, the angle measured corresponds to the tilt. In the roll condition, the rocket moving from launch to landing shows the rocket's rotational motion at an angle of approximately 20o. The potential of water rockets that can still be developed, needs to be increased the reliability of water rockets both in terms of utilization and research.
Co-Authors Aji Nur Rizki Apik Rusdiarna I.P Apik Rusdiarna Indra Praja Ardi, Subhan Zul Damar Yoga Kusuma Hariyadi Soetedjo Hilmi, Isom I.P, Apik Rusdiarna Kusuma, Damar Yoga Lita Indriastika Margi Sasono Rahmadhia, Safinta Nurinda Rizki, Aji Nur Sri Handayaningsih Subhan Zul Ardi Suwartiningsih, Nurul umi salamah Umi Salamah Yuda Wiges Pratama