AEROENG 4518
Transcript Abbreviation:
Des Spc Veh Sys II
Course Description:
Continuation of 4517: Preliminary and detailed design of space vehicle components. Design of a space vehicle/system, and mission scenarios simulation via computer software.
Course Levels:
Undergraduate (1000-5000 level)
Designation:
Required
General Education Course
(N/A)
Cross-Listings
(N/A)
Credit Hours (Minimum if “Range”selected):
3.00
Max Credit Hours
(N/A)
Select if Repeatable:
Off
Maximum Repeatable Credits
(N/A)
Total Completions Allowed
(N/A)
Allow Multiple Enrollments in Term:
No
Course Length:
14 weeks (autumn or spring)
12 weeks (summer only)
Off Campus:
Never
Campus Location:
Columbus
Instruction Modes:
In Person (75-100% campus; 0-24% online)
Prerequisites and Co-requisites:
Prereq: 4517, and enrollment as AeroEng-BS student (No pre-majors can enroll in this course).
Electronically Enforced:
No
Exclusions
(N/A)
Course Goals / Objectives:
Provide students with conceptual and detailed spacecraft design experience
Foster multidisciplinary thought processes and collaborations
Train students in effective teamwork
Refine students' technical communication skills through written reports and presentations
Teach students the importance of considering engineering standards in the design process.
Check if concurrence sought:
No
Contact Hours:
| Topic | LEC | REC | LAB | LAB Inst |
|---|---|---|---|---|
| Minimum Buckling Load Design FEA with Hypermesh and Nastran contdChp 3 (FEA - Truss, Beam and Frame Structures), Frame and Rotating Beam | 2.5 | 0 | 5 | 0 |
| Low Cycle/High Cycle Fatigue Design FEA with Hypermesh and Nastran Chp 4: FEA - Plates and Shells | 2.5 | 0 | 5 | 0 |
| FEA with Hypermesh and Nastran Chps 5, 6: FEA - Solid Bodies | 2.5 | 0 | 5 | 0 |
| Structural Integration and component mode synthesis of rigid and flexible appendages to main flight vehicle body for total vehicle structural dynamic analysis and design | 2.5 | 0 | 5 | 0 |
| Structural Integration – component mode synthesis -continued Structural design Progress report (PR1) | 2.5 | 0 | 5 | 0 |
| Spacecraft maneuver and attitude dynamics and control system design; actuators and sensors; pulsewidth modulation; launch-onorbit operational modes, planet and sun acquisition; momentum dumping; closed-loop attitude simulation | 8 | 0 | 15 | 0 |
| Cost analysis and estimation methods, assesment of space environment Progress report Presentation (PRP2) | 2.5 | 0 | 5 | 0 |
| STK/ODTK, MATLAB, MATLAB SIMULINK: orbit, attitude, propulsion, power, communication subsystems, coverage and access, sensors integration; space weather ANSYS, NX-IDEAS: structural and thermal analysis of configuration | 13 | 0 | 26 | 0 |
| Final Year –end design report and presentations, submission of poster (FYR) | 3.0 | 0.0 | 6 | 0 |
| Total | 39 | 0 | 77 | 0 |
Grading Plan:
Letter Grade
Course Components:
Lecture
Lab
Grade Roster Component:
Lecture
Credit by Exam (EM):
No
Grades Breakdown:
| Aspect | Percent |
|---|---|
| Progress Reports 1 | 15% |
| Progress Reports 2 | 15% |
| Final Oral Presentation | 20% |
| Final Design Poster | 20% |
| Final Formal Report | 30% |
Representative Textbooks and Other Course Materials:
| Title | Author | Year |
|---|---|---|
| Space Mission Engineering: The New SMAD, Space Technology Library, Vol. 28 | James M. Wertz (editor) | 2011 |
| Space Vehicle Design (Second Edition), AIAA Publishing, ISBN 1-56347-539-1 | Michael D. Griffin and James R. French | 2004 |
| Spacecraft Systems Engineering (Fourth Edition), John Wylie and Sons, ISBN 978-0-470-75012-4 | Peter Fortescue, Graham Swinerd, John Stark (Editors | 2011 |
ABET-CAC Criterion 3 Outcomes
(N/A)
ABET-ETAC Criterion 3 Outcomes
(N/A)
ABET-EAC Criterion 3 Outcomes:
| Outcome | Contribution | Description |
|---|---|---|
| 1 | Significant contribution (7+ hours) | an ability to identify, formulate, and solve complex engineering problems by applying principles of engineering, science, and mathematics |
| 2 | Significant contribution (7+ hours) | an ability to apply engineering design to produce solutions that meet specified needs with consideration of public health, safety, and welfare, as well as global, cultural, social, environmental, and economic factors |
| 3 | Significant contribution (7+ hours) | an ability to communicate effectively with a range of audiences - pre-2019 EAC SLO (g) |
| 4 | Substantial contribution (3-6 hours) | an ability to recognize ethical and professional responsibilities in engineering situations and make informed judgments, which must consider the impact of engineering solutions in global, economic, environmental, and societal contexts |
| 6 | Significant contribution (7+ hours) | an ability to develop and conduct appropriate experimentation, analyze and interpret data, and use engineering judgment to draw conclusions |
| 7 | Substantial contribution (3-6 hours) | an ability to acquire and apply new knowledge as needed, using appropriate learning strategies |
Embedded Literacies Info:
Advanced Writing
1.1 Investigate and integrate knowledge of the subject, context and audience with knowledge
1.2 Use of genres, conventions and rhetorical choices to advance a particular writing objective
2.1 Use credible and relevant sources of information, evaluate assumptions, and consider alternative viewpoints or hypotheses to express ideas and develop arguments
2.2 Reflect on how they adapt rhetorical and research strategies they have learned to contexts
2.3 Develop scholarly, creative or professional products that are meaningful to them and their audience
Data Analysis - Quantitative
1.4A Evaluate the social and ethical implications of data collection and analysis, especially in relation to human subjects
Technology
1.1 Critically describe the relationships between technology and society in historical and cultural context
1.2 Recognize how technologies emerge and change
1.3 Evaluate the social and ethical implications of technology
Attachments
(N/A)
Additional Notes or Comments
(N/A)