RANCANG BANGUN SISTEM PELONTAR TIPE CATAPULT UNTUK WAHANA TERBANG TIPE FIXEDWING ATHA MAPPER 2300
DOI:
https://doi.org/10.24853/jurtek.15.1.13-24Keywords:
Atha Mapper 2300, Sistem Pelontar, Catapult, LauncherAbstract
Atha Mapper 2300 is a fixed wing aircraft, which is the next generation of Atha Mapper 2150. In order to finish its mission, the aircraft used to take off by hand launch method. Hand launch method utilize the throwing force of the launch operator to take off. The method has many issues, such as low safety degree, and inconsistent take off angle and speed. The purpose of this research are to design a launcher for Atha Mapper 2300 UAV, to determine the structural strength for Atha Mapper 2300 launcher system, to produce the designed launcher system, and to find out the performance of the produced launcher system. The design process was based on the Atha Mapper 2300 specification, which are 2300 mm of wingspan, MTOW: 6 Kg, and 10 m/s of stall speed. The result of the design was a launcher system with dimension of 3000 mm length, 1400 mm wide, 900 mm height, and 14o inclination angle. The launcher system was a catapult type launcher with 30 x 60 x 1.2 mm hollow stainless steel as its main material, and has a total mass of 11.162 Kg. The structural strength calculation resulted a criteria fulfillment of 113.4. The calculation also resulted a maximum launch speed of 11.658 m/s. Then, practically the produced launcher result a maximum launch speed of 12.116 m/s which is relatively close to the theoretical calculation. The speed fulfill the initial criteria which is ≥ 11.5 m/s. By these results, the launcher system was claimed to be successfully help Atha Mapper 2300 to have a stabilized take off.Downloads
References
Anuar, K., Akbar, M., & Herisiswanto. (2019). Wing design of uav serindit v-1. IOP Conference Series: Materials Science and Engineering, 539, 012002. https://doi.org/10.1088/1757-899x/539/1/012002
Anuar, K., Fatra, W., & Akbar, M. (2020). Tricopter Vehicle Frame Structure Design Integrated as Platform of Fixed Wing Atha Mapper 2150. 64(2), 68–72. https://doi.org/http://dx.doi.org/10.36842/jomase.v64i2.218
Budynas, R., & Keith, N. (2015). Mechanical Engineering Design. Mc Graw Hill.
Corda, S. (2017). (Aerospace Series) Pascual Marqués, Andrea Da Ronch - Advanced UAV Aerodynamics, Flight Stability and Control_ Novel Concepts, Theory and Applications-John Wiley & Sons, Inc. (2017).pdf. Wiley.
Fahlstrom, P. G., & Gleason, T. J. (2012). Introduction to UAV Systems (First edit). John Wiley & Sons Ltd. https://doi.org/10.1002/9781118396780
Laka, O., Nazaruddin, & Syafri. (2018). Perancangan dan Analisis Statik Sistem Rangka Mobil Hemat Energi Asykar Hybrid Universitas Riau. Jom FTEKNIK, 5(2), 1–6. https://www.researchgate.net/profile/Nazaruddin_Nazaruddin/publication/341895049_PERANCANGAN_DAN_ANALISIS_STATIK_SISTEM_RANGKA_MOBIL_HEMAT_ENERGI_ASYKAR_HYBRID_UNIVERSITAS_RIAU/links/5ed84ddf92851c9c5e7b877f/PERANCANGAN-DAN-ANALISIS-STATIK-SISTEM-RANGKA-M
Lu, Y., Chen, Q., Jia, G., & Guo, Z. (2020). Development and experiment of elastic-rope launcher for small fixed-wing UAVs. Proceedings - 2020 3rd World Conference on Mechanical Engineering and Intelligent Manufacturing, WCMEIM 2020, 654–658. https://doi.org/10.1109/WCMEIM52463.2020.00142
Miller, B., Valoria, C., Warnock, C., & Coutlee, J. (2014). Lightweight UAV Launcher Senior Project for Aerojet--Rocketdyne Final Report Team Rocket Power.
Muliadi, J. (2018). An empirical method for the catapult performance assessment of the BPPT-developed UAVs. Journal of Physics: Conference Series, 1130(1). https://doi.org/10.1088/1742-6596/1130/1/012033
Nazaruddin, N., Adhitya, M., Sumarsono, D. A., Heryana, G., Siregar, R., Prasetya, S., & Zainuri, F. (2021). Development of Electric Vehicle (ev)-Bus Chassis with Reverse Engineering Method Using Static Analysis. Eastern-European Journal of Enterprise Technologies, 2, 15–22. https://doi.org/10.15587/1729-4061.2021.219928
Nazaruddin, N., Zainuri, F., Prasetya, S., Siregar, R., Heryana, G., Adhitya, M., & Sumarsono, D. A. (2020). Development of leaf spring design in large vehicles made from material type 65 si7 using static analysis with reverse engineering. IOP Conference Series: Materials Science and Engineering, 909(1). https://doi.org/10.1088/1757-899X/909/1/012022
Novaković, Z., & Medar, N. (2013). Analysis of a UAV Bungee Cord Launching Device. In Scientific Technical Review (Vol. 63, Issue 3).
S.M. Woo, D.H. Kim, Y. R. K. (2021). InvestigationofStallPreventionConditionforaHand-LaunchedUAVusingComputationalFluidDynamics (pp. 84–93). Journal Of Computational Fluids Engineering 26.2 (2021): 84-93.
Sadraey H, M. (2020). Design of Unmanned Aerial Systems (First Edit). John Wiley & Sons Ltd.
Soetanto, M. F., & Tritjahjono, R. I. (2016). Study the Strength of Material and Composite Structures of Belly-Landing Mini UAV. Applied Mechanics and Materials, 842, 178–185. https://doi.org/10.4028/www.scientific.net/amm.842.178
Downloads
Published
How to Cite
Issue
Section
License
COPYRIGHT POLICY
The author(s) of an article published in the Jurnal Teknologi retains ownership of the intellectual property rights in work (s).
PUBLISHING RIGHTS
The author(s) of an article published in the Jurnal Teknologi have unrestricted publication rights. The authors give the Jurnal Teknologi the right to publish the article and designate the Faculty of Engineering Universitas Muhammadiyah Jakarta Publishing as the original publisher of the article.
LICENSING POLICY
Journal of Mechanical Engineering and Sciences is an open-access journal that follows the Creative Commons Non-Commercial 4.0 International License (CC BY-NC 4.0), which states that:
Under this license, the reusers must give appropriate credit, provide a link to the license, and indicate if changes were made. Users may do so in any reasonable manner, but not in any way that suggests the licensor endorses users or their use.
Please take the time to read the whole license agreement (https://creativecommons.org/licenses/by-nc/4.0/). As long as reusers follow the license conditions, the owner cannot withdraw these freedoms. The following components are included under this license:
Attribution: Users must provide appropriate attribution, including a link to the license, and indicate whether or not they made any modifications. Users are free to do so reasonably, but not in a manner that indicates the licensee approves of their usage.
NonCommercial: Users may not use the material for commercial purposes.