@thesis{thesis,
		author={DWI SAPUTRA  FEBRY},
		title ={ANALISIS PERBANDINGAN FUEL METHANOL-MINYAK JARAK DAN NITRO 30% PADA ENGINE OS 25 LA UNTUK UJI THRUST MENGGUNAKAN PROPELLER APC 9 X 5},
		year={2024},
		url={http://eprints.stta.ac.id/1709/},
		abstract={This study examines the effect of using alternative fuels, specifically 
methanol and nitromethane (30%), on the engine of an OS 25 LA remote control 
(RC) airplane model. Methanol, as a fuel that can be produced from renewable 
resources, provides the potential to reduce dependence on fossil fuels. Nitro (30%) 
has specific properties that improve engine performance, especially Thrust and 
propeller rotation. This experimental study aims to understand the effect of both 
fuels on the Thrust and propeller rotation of an OS 25 LA engine. Results show that 
nitro fuel (30%) produces higher Thrust (1,464 N) and faster propeller rotation 
(11,325) compared to methanol-castor oil. Combustion efficiency was also higher 
in nitro (30%) (18%), indicating more optimal fuel energy utilization. Thus, the use 
of nitro (30%) can be considered as a more efficient and quality fuel option to 
improve the performance of the RC OS 25 LA engine.}
		}