RT info:eu-repo/semantics/bachelorThesis
T1 Diseño de misiles tierra-aire de larga distancia utilizando diferentes sistemas propulsivos
T2 Long-range surface-to-air missile design using different propulsive systems
A1 Doncel del Amo, David
A2 Ingenieria Aeroespacial
K1 Ingeniería aeroespacial
K1 Motor cohete
K1 Estetoreactor
K1 Aerodinámica
K1 Propulsión
K1 Misiles tierra-aire
K1 3301.15 Sistemas de Propulsión
K1 3324 Tecnología del Espacio
AB [EN] The purpose of this project is to design two surface-to-air missiles able to intercept a target moving at a maximum speed of Mach 1, 200 kilometers away from the launch point and 20 kilometers above sea level. Each one will be powered differently. One of them will use only rocket motors while the other will be powered by a ramjet so it will be possible to observe how each propulsive system is integrated into the missile, how it affects its performance and what advantages or limitations each one has. Furthermore, the design of the different subsystems that shape the missile will be detailed, adapting it to the needs of both missiles. The ramjet missile turns out to be faster, and its dimensions are much smaller. This missile intercepts the target in 190 seconds, its weight is 976 kilograms, and its length is 5.1 meters. The rocket missile, thanks to its two solid propellant stages, is able to intercept the target in 219 seconds. Its weight is 2214 kilograms, and its length is 8 meters. Both missiles have a diameter of 0.5 meters to facilitate their comparison. The rocket motor missile’s flight ceiling is 32 kilometers, while the ramjet missile has a ceiling of 20 kilometers, limited by its own propulsive characteristics. Both missiles have been compared with other similar missiles already on use to ensure the most realistic design possible. The result of the comparison is positive, as both designs are within expectations.
LK https://hdl.handle.net/10612/21554
UL https://hdl.handle.net/10612/21554
NO Doncel del Amo, D. (2023). Diseño de misiles tierra-aire de larga distancia utilizando diferentes sistemas propulsivos. [Trabajo de fin de Grado, Universidad de León]
DS BULERIA. Repositorio Institucional de la Universidad de León
RD Jul 17, 2024