Checking date: 26/04/2024


Course: 2024/2025

Advanced Space Propulsion
(18583)
Master in Aeronautical Engineering / Máster Universitario en Ingeniería Aeronáutica (Plan: 328 - Estudio: 296)
EPI


Coordinating teacher: AHEDO GALILEA, EDUARDO ANTONIO

Department assigned to the subject: Aerospace Engineering Department

Type: Compulsory
ECTS Credits: 3.0 ECTS

Course:
Semester:




Requirements (Subjects that are assumed to be known)
Design of Space Systems
Objectives
The course is focused on Electric Space Propulsion, as the new leading technology for in-space propulsion both in Near-Earth and Inner-Solar system applications. The goals of the course are that the students acquire a solid understanding of - the benefits and limitations of electric rocket propulsion versus classical chemical rocket propulsion, for different missions, and from microsatellites to large platforms. - the different types of electric thrusters and their main principles of operations - the main plasma physics concepts inherent to these thrusters - the derivation of performance models to support design, testing, and optimization of these technologies - the main technological constraints found in practice
Skills and learning outcomes
Description of contents: programme
1. INTRODUCTION TO IN-SPACE PROPULSION Propulsion figures of merit: thrust, specific impulse, efficiencies. Propulsive requirements in space missions. Rocket equation. Chemical versus electric propulsion 2. CHEMICAL PROPULSION IN SPACE Figures of merit in chemical rockets (nozzles): thrust coefficient, characteristic velocity, etcetera. Monopropellant rockets: cold gas and hydrazine-based rockets. Bipropellant rockets: analysis of fuels and oxidizers. Review of thermochemistry. 3. PLASMA PROPULSION PHYSICS Operation principles of Ion and Hall Thrusters. Maxwell and Fluid equations. Collisional processes. Quasineutrality, Debye sheaths, and plasma wall interaction. Dynamics of magnetized populations. 4. GRIDDED ION THRUSTERS Thruster elements and electrical configuration. Global model of the discharge chamber: current and power balances. Grid model: Child model and optimal perveance Model of expansion of the plasma jet. Performance laws and efficiencies. Physics of the hollow cathode: thermionic emission. Thruster lifetime. 5. HALL EFFECT THRUSTERS Plasma discharge structure and operational parameters. Global model: current and energy balances, efficiencies. Axial and radial fluid models: electron transport, interaction with walls. Technological aspects: chamber erosion, thermal loads, oscillations, magnetic circuit and topology. Alternative configurations. 6. PLASMA DIAGNOSTICS AND TESTING Vacuum facilities, and test bench. Physics of electrostatic diagnostics: Faraday probes and performance assessment Test plan and test report.
Learning activities and methodology
They combine - lectures with audiovisual support - discussion and solving of exercises and problems - session in laboratory - quizzes Tutorials can be both personally or through Aula Global
Assessment System
  • % end-of-term-examination 60
  • % of continuous assessment (assigments, laboratory, practicals...) 40

Calendar of Continuous assessment


Basic Bibliography
  • D. GOEBEL, I. KATZ. FUNDAMENTALS OF ELECTRIC PROPULSION 2ND EDITION. WILEY. 2024
  • G.P. SUTTON, O. BIBLARZ. ROCKET PROPULSION ELEMENTS, 9TH EDITION. WILEY. 2001
  • R. JAHN. PHYSICS OF ELECTRIC PROPULSION. DOVER. 2006

The course syllabus may change due academic events or other reasons.