Proyecto final de Grado: Diseño y análisis de un sistema de propulsión para CubeSats basado en vapor sobrecalentado =
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2022
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"En este trabajo se diseña un sistema de propulsión orbital de gas caliente del tipo Resisto-Jet a a base de agua, para su implementación en Cube-yMicroSats de al menos 6U, como sistema de maniobra orbital. Se busca obtener un dispositivo auto contenido en 1U, con un tanque autopresurizado de agua líquida al momento de operación, que evite la introducción de bombas o de sistemas de presurización externa. Se busca minimizar la utilización de partes móviles, y el uso de materiales tóxicos o restringidos."
"An H2O ResistoJet type propulsion system is designed for its use in CubeSats larger than 6U as an orbital maneuvering system. Designed to be self-contained in one unit, its electrically heated evaporator, and auperheater systems are fed by a self-pressurized liquid water tank,thus characterized by its simplicity due to the lack of pumps or external pressurizing systems. Moving parts and the use of toxic materials are minimized."
"An H2O ResistoJet type propulsion system is designed for its use in CubeSats larger than 6U as an orbital maneuvering system. Designed to be self-contained in one unit, its electrically heated evaporator, and auperheater systems are fed by a self-pressurized liquid water tank,thus characterized by its simplicity due to the lack of pumps or external pressurizing systems. Moving parts and the use of toxic materials are minimized."
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PROPULSION, SATELITES, MONOPROPELENTES