Bachelor of Science in Aerospace Engineering
The field of aerospace engineering developed because of humanity’s desire for aircraft systems for military, commercial, and civilian purposes; it was first called aeronautical engineering or aeronautics. When the space age began, it was natural for aeronautical engineers to participate in the development of spacecraft systems for space exploration. This branch of engineering became known as astronautical engineering or astronautics, and the combined field is called aerospace engineering or aeronautics and astronautics. Because of the diverse nature of the work, the aerospace engineer must have a basic knowledge of physics, mathematics, digital computation, and the various disciplines of aerospace engineering: aerodynamics and propulsion, structural mechanics, flight mechanics and orbital mechanics, and control. Because of their extensive education in fundamental disciplines, aerospace engineers can work in areas other than aerospace engineering and are employed in a wide range of careers.
The objectives of the aerospace engineering degree program are to prepare students for professional practice in aerospace engineering and related engineering and scientific fields; to prepare students for such postbaccalaureate study as their aptitudes and professional goals may dictate; to instill in students a commitment to lifelong education and to ethical behavior throughout their professional careers; and to make students aware of the global and societal effects of technology. To meet these objectives, the faculty has designed a rigorous curriculum that emphasizes fundamentals in the basic sciences, mathematics, and the humanities, and integrates classroom and laboratory experiences in the engineering disciplines of aerodynamics and propulsion, structural mechanics, mechanics of materials, flight and orbital mechanics, controls, computation, electromechanical systems, design, and technical communication. The curriculum requires students to use modern engineering tools, to work individually, and to practice teamwork.
The first two years of the aerospace engineering curriculum emphasize fundamental material along with engineering sciences, while the third year introduces concepts in the areas of fluid mechanics, structural mechanics, system dynamics and control, and experimentation. The fourth year provides further depth in aerospace engineering, with emphasis on design and laboratory courses. During the junior year, the student elects to pursue one of two technical areas, atmospheric flight or space flight. Both area options are complemented by general education courses and courses offered in other engineering disciplines. In addition, the student may choose technical electives that increase the breadth of the program or that provide additional depth within one or more subdisciplines within the department. All of the following subdisciplines are also represented in the required courses for both technical area options.
Aerodynamics and Propulsion
This subdiscipline involves fluid motion, propulsion, lift and drag on wings and other bodies, high-speed heating effects, and wind tunnel investigation of these problems. Topics of study include fluid mechanics, gas dynamics, heat transfer, aerodynamics, propulsion, computational fluid dynamics, and experimental fluid mechanics.
This subdiscipline includes the study of airplane, spacecraft, and missile structures, the materials that make them efficient, and methods for testing, analysis, and design of new structural systems. Course topics include structural analysis, structural dynamics, materials (including advanced composites), aeroelasticity, experimental structural mechanics, and computer-aided design of structures.
Flight Mechanics and Orbital Mechanics
Flight mechanics involves the analysis of the motion of aircraft, missiles, rockets, reentry vehicles, and spacecraft that are subjected to gravitational, propulsive, and aerodynamic forces; the study of uncontrolled motion of satellites and coasting spacecraft is usually referred to as orbital mechanics. Subject matter in these areas includes trajectory analysis and optimization; attitude dynamics, stability, and control; flight test; orbit determination; orbital operations; systems engineering; sensors; satellite hardware applications; and simulation.
Control theory is applied in aerospace engineering to the development of automatic flight control systems for aircraft (autopilots and stability augmentation systems), attitude control systems for satellites, and guidance and control systems for missiles, rockets, reentry vehicles, and spacecraft. Course topics include linear system theory, classical control theory, digital control, and probability theory.
Portable Computing Devices
Students entering aerospace engineering are required to have access to a portable computing device capable of running the software tools required for undergraduate engineering analyses (MATLAB, SOLIDWORKS, Word, Excel, etc.) and accessing the remote server for the department. This device does not need to be brought to campus on a daily basis, but individual courses may require that the device be brought to certain lectures, labs, and/or exams. Minimum and recommended specifications may be found on the department website.
Course requirements include courses within the Cockrell School of Engineering and other required courses. In addition, each student must complete the University’s Core Curriculum. In some cases, a course that fulfills one of the following requirements may also be counted toward Core Curriculum or flag requirements; these courses are identified below.
In the process of fulfilling engineering degree requirements, students must also complete coursework to satisfy the following flag requirements: one independent inquiry flag, one quantitative reasoning flag, one ethics flag, one global cultures flag, one cultural diversity in the United States flag, and two writing flags. The independent inquiry flag, the quantitative reasoning flag, the ethics flag, and both writing flags are carried by courses specifically required for the degree; these courses are identified below. Courses that may be used to fulfill flag requirements are identified in the Course Schedule.
Courses used to fulfill technical elective requirements must be approved by the aerospace engineering faculty before the student enrolls in them.
The student must take all courses required for the degree on the letter-grade basis and must earn a grade of at least C- in each course, except for those listed as Remaining Core Curriculum courses. He or she must also maintain grade point averages of at least 2.00 in the major area of study and in required technical courses as described in Academic Standards, and a cumulative University grade point average of at least 2.00 as described in General Information.
|Aerospace Engineering Courses|
|ASE 120K||Low-Speed Aerodynamics Laboratory||1|
|ASE 320||Low-Speed Aerodynamics||3|
|ASE 324L||Aerospace Materials Laboratory||3|
|ASE 330M||Linear System Analysis||3|
|ASE 333T||Engineering Communication (writing flag and ethics flag)||3|
|ASE 362K||Compressible Flow||3|
|ASE 366K||Spacecraft Dynamics||3|
|ASE 367K||Flight Dynamics||3|
|ASE 370C||Feedback Control Systems||3|
|ASE 375||Electromechanical Systems||3|
|CH 301||Principles of Chemistry I (part II science and technology)||3|
|COE 301||Introduction to Computer Programming||3|
|COE 311K||Engineering Computation||3|
|E M 306||Statics||3|
|E M 311M||Dynamics||3|
|E M 319||Mechanics of Solids||3|
|M 408C||Differential and Integral Calculus (mathematics; quantitative reasoning flag)||4|
|M 408D||Sequences, Series, and Multivariable Calculus||4|
|M 427J||Differential Equations with Linear Algebra (quantitative reasoning flag)||4|
|or M 427K||Advanced Calculus for Applications I|
|M 427L||Advanced Calculus for Applications II||4|
|PHY 103M||Laboratory for Physics 303K||1|
|PHY 103N||Laboratory for Physics 303L||1|
|PHY 303K||Engineering Physics I (part I science and technology; quantitative reasoning flag)||3|
|PHY 303L||Engineering Physics II (part I science and technology; quantitative reasoning flag)||3|
|Rhetoric and Writing|
|RHE 306||Rhetoric and Writing (English composition)||3|
|Other required courses|
|Technical area courses||13|
|Approved technical electives||6|
|M E 210||Engineering Design Graphics||2|
|M E 310T||Applied Thermodynamics||3|
|Remaining Core Curriculum Courses|
|E 316L||British Literature 1||3|
|or E 316M||American Literature|
|or E 316N||World Literature|
|or E 316P||Masterworks of Literature|
|American and Texas government 2||6|
|American history 2||6|
|Social and behavioral sciences 3||3|
|Visual and performing arts 3||3|
|UGS 302||First-Year Signature Course 4||3|
|or UGS 303||First-Year Signature Course|
|1. Some sections of the English humanities courses (E 316L, 316M, 316N, 316P) carry a global cultures or cultural diversity flag.|
|2. Some sections carry a cultural diversity flag.|
|3. Some sections carry a global cultures and/or cultural diversity flag.|
|4. In UGS 302, all sections carry a writing flag. In UGS 303, some sections carry a writing flag.|
Technical Area Options
The technical area option allows the student to choose 13 semester hours of technical area courses in either atmospheric flight or space flight. Each student should choose a technical area by the end of the first semester of the junior year and plan an academic program to meet the area requirements in the next three semesters. Many students choose technical electives that will strengthen their backgrounds in one specialty area, but this is not required. It should be noted that a student may choose the technical area courses in the other technical area as technical electives.
Area 1, Atmospheric Flight
Also called aeronautics, this area provides the student with a well-rounded program of study emphasizing the major disciplines of aerodynamics, propulsion, structures, design, performance, and control of aircraft. These subjects are treated at a fundamental level that lays a foundation for work in a broad variety of specialties in the aircraft industry. This option is intended for the undergraduate student whose primary interest is aircraft.
Computational Engineering 321K, Computational Methods for Structural Analysis
Aerospace Engineering 361K, Aircraft Design I (carries an independent inquiry flag)
Aerospace Engineering 361L, Aircraft Design II (carries a writing flag)
Aerospace Engineering 162M, High-Speed Aerodynamics Laboratory
Aerospace Engineering 364, Applied Aerodynamics
Area 2, Space Flight
Also called astronautics, this area offers a well-rounded program of study that provides a background in the traditional areas of fluid mechanics, materials, structures, propulsion, controls, and flight mechanics, while also giving the student a chance to learn about the space environment, attitude determination and control, orbital mechanics, mission design, and spacecraft systems engineering. These subjects are treated at a fundamental level that lays a foundation for work in a broad variety of specialties in space-related industries. This option is intended for the undergraduate student whose primary interest is space and spacecraft.
Aerospace Engineering 366L, Applied Orbital Mechanics
Aerospace Engineering 166M, Spacecraft Systems Laboratory
Aerospace Engineering 372K, Attitude Dynamics
Aerospace Engineering 374K, Space Systems Engineering Design
Aerospace Engineering 374L, Spacecraft/Mission Design (carries an independent inquiry flag and a writing flag)
The degree requires all students to take three semester hours of an approved structures elective.
Students pursuing the Technical Area 1, Atmospheric Flight, must take Aerospace Engineering 365, Structural Dynamics, to fulfill this requirement.
Students pursuing Technical Area 2, Space Flight, will choose one of four options to fulfill this requirement:
Aerospace Engineering 339/Engineering Mechanics 339, Advanced Strength of Materials
Aerospace Engineering 357, Mechanics of Composite Materials
Aerospace Engineering 365, Structural Dynamics
Computational Engineering 321K, Computational Methods for Structural Analysis.
Special Projects Laboratories
The department offers students the opportunity to participate in special projects such as student-built radio-controlled aircraft competitions and student satellite-building projects. These time-intensive projects are open to all aerospace engineering students with at least 15 semester hours of University credit toward the degree and a grade point average of at least 2.50. Academic credit for participation in departmentally approved student projects is available on the pass/fail basis through the course Aerospace Engineering 128. Three such laboratory courses can be combined to count as one three-hour technical elective; one such laboratory course can be combined with a two-hour cooperative program to count as one three-hour technical elective.