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
Check if concurrence sought:
No
Contact Hours:
| Topic | LEC | REC out-of-class | REC in-class | Weekly LAB out-of-class | Weekly LAB in-class |
|---|---|---|---|---|---|
| Minimum Buckling Load Design FEA with Hypermesh and Nastran contdChp 3 (FEA - Truss, Beam and Frame Structures), Frame and Rotating Beam | 3.0 | 3.0 | 0 | 0.0 | 0 |
| Low Cycle/High Cycle Fatigue Design FEA with Hypermesh and Nastran Chp 4: FEA - Plates and Shells | 3.0 | 3.0 | 0 | 0.0 | 0 |
| FEA with Hypermesh and Nastran Chps 5, 6: FEA - Solid Bodies | 3.0 | 3.0 | 0 | 0.0 | 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 | 3.0 | 3.0 | 0 | 0.0 | 0 |
| Structural Integration – component mode synthesis -continued Structural design Progress report (PR1) | 3.0 | 3.0 | 0 | 0.0 | 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 | 9.0 | 9.0 | 0 | 0.0 | 0 |
| Cost analysis and estimation methods, assesment of space environment Progress report Presentation (PRP2) | 3.0 | 3.0 | 0 | 0.0 | 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 | 15.0 | 15.0 | 0 | 0.0 | 0 |
| Final Year –end design report and presentations, submission of poster (FYR) | 3.0 | 0.0 | 0 | 0.0 | 0 |
| Total | 45 | 42 | 0 | 0 | 0 |
Grading Plan:
Letter Grade
Course Components:
Lecture
Recitation
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 |
|---|---|---|
| Satellite Communications Systems (SCS) - by ,- 4th Edition, John Wiley | Gerard Maral and Michel Bousquet | |
| Space Mission Analysis and Design, and SMAD Workbook III, Microcosm, Inc., Torrance, CA and Kluwer Academic Publishers, Boston, MA, 1991. | Larson and Wertz, | |
| Spacecraft Structures and Mechanisms by Microcosm Press | Sarafin (editor) |
ABET-CAC Criterion 3 Outcomes:
(N/A)
ABET-ETAC Criterion 3 Outcomes:
(N/A)
ABET-EAC Criterion 3 Outcomes:
| Significant contribution (7+ hours) | 1 | an ability to identify, formulate, and solve complex engineering problems by applying principles of engineering, science, and mathematics |
| Significant contribution (7+ hours) | 2 | 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 |
| Significant contribution (7+ hours) | 3 | an ability to communicate effectively with a range of audiences - pre-2019 EAC SLO (g) |
| Substantial contribution (3-6 hours) | 4 | 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 |
| Significant contribution (7+ hours) | 6 | an ability to develop and conduct appropriate experimentation, analyze and interpret data, and use engineering judgment to draw conclusions |
| Substantial contribution (3-6 hours) | 7 | an ability to acquire and apply new knowledge as needed, using appropriate learning strategies |
Embedded Literacies Info: