![]() Participation in ASTE undergraduate student team projects. Two-body motion, rigid-body motion, attitude dynamics and maneuvers, spacecraft stabilization: gravity gradient, reaction wheels, magnetic torques, thruster attitude control. Prerequisite: PHYS 152 and (ASTE 305 or AME 309). Liquid-fueled and solid-fueled rocket engines adiabatic flame temperature duct flows with area change, heat addition, mass addition rocket heat transfer staging and electric thrusters. Prerequisite: senior or graduate standing. Recommended preparation: AME 309 or ASTE 301b. Physical description of kinetic nature of gas flows distribution function introduction to the Boltzmann equation free-molecular flow surface and molecular reflection properties Monte Carlo flow calculations. Senior standing.ĪSTE 445 Molecular Gas Dynamics (3 units) The mission specification will be different each year. Competing teams of 5-6 students, depending on total course enrollment, will respond to an instructor-provided mock-RFP for a space system. Recommended preparation: Basic programming experience with Matlab, C/C++, Python, or other programming languages, and/or similar exposure on the level of ITP 115 or ITP 165.Ĭapstone, team-oriented space systems design course. Prerequisite: ASTE 280 corequisite: PHYS 153L recommended preparation: Skill in MATLAB programming and spreadsheets.ĪSTE 404 Computational Programming and Numerical Methods (3 units)ĭevelopment of simulation code with high-performance languages such as C++ and Fortran numerical techniques for continuum and rarefied gas flows, GPU utilization data visualization, machine learning. Systems engineering as applied to spacecraft. Introduction to spacecraft systems: propulsion, attitude dynamics and control, structures, communications, power, thermal control. Prerequisite: ASTE 280, PHYS 153L.ĪSTE 331ab Spacecraft Systems Engineering (3 units, 3 units) Space environment: atmosphere, gravity gradients, radiation. Spacecraft systems: attitude determination and control, power, thermal, command and data handling, telecommunication, structures and mechanisms, propulsion. Prerequisite: (PHYS 153L or PHYS 163L) and AME 310 corequisite: MATH 245.ĪSTE 330 Introduction to Spacecraft Systems and the Space Environment (3 units) Introduction to compressible and rarefied gas flows with applications to rocket propulsion and the dynamics of supersonic and hypersonic vehicles and spacecraft ionized gases and plasmas. Prerequisite: MATH 245, PHYS 153L.ĪSTE 305 Astronautical Gas Dynamics (4 units) Thermodynamics and statistical mechanics kinetics of atoms, molecules, and photons compressible fluid dynamics. Intended for lower-division students or those with little prior project experience.ĪSTE 301ab Thermal and Statistical Systems (3 units, 3 units) Introduction to rocket propulsion, spacecraft attitude dynamics and control, and space environment. ![]() Laboratory: IntroductionĪSTE 280 Foundations of Astronautical Engineering (3 units)Ĭoordinate systems and transformations. Elements of orbits, spacecraft systems, rocket Introduction to space, space exploration and the spaceīusiness. Gateway to the major in Astronautical Engineering. With that in the Catalogue, the Catalogue must be consideredĪSTE 101L Introduction to Astronautics (4 units) In the event that information on this website conflicts The USC Catalogue is the official source of information
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