, and engaging her students with interactive methods.Mr. David B Kanipe, Texas A&M University After receiving a BS in Aerospace Engineering in May 1970, followed by a MS in Aerospace Engineering in August 1971 from Texas A&M University, Mr. Kanipe accepted a position with NASA at the Manned Spacecraft Center in Houston and began his professional career in November 1972. A month after his arrival at NASA, the last Apollo mission, Apollo 17, was launched. Obviously, that was exciting, but in terms of his career, the commencement of the Space Shuttle Program in November 1972 was to have far more impact. As a result, David was able to begin his career working on what he says was the most interesting and
administration of the persistence in engineering survey. Journal of Engineering Education, 99(4), 371-395. 7. Lichtenstein, G., Loshbaugh, H. G., Claar, B., Chen, H. L., Jackson, K., & Sheppard, S. D. (2009). An engineering major does not (necessarily) an engineer make: Career decision making among undergraduate engineering majors. Journal of Engineering Education, 98(3), 227-234. 8. Committee on the National Aerospace Initiative, Air Force Science and Technology Board Division on Engineering and Physical Sciences. (2004). Evaluation of the National Aerospace Initiative. Washington, DC: National Academies Press. 9. Weigel, A. (2010). “Survey of aerospace student attitudes.” Retrieved February 20, 2011
configuration of a helicopter for a given mission. 12. The student shall plan for flight test of total performance of a helicopter. 13. The student shall measure performance of a helicopter in a flight test. Page 26.840.10 B. Tool - Mapping the Learning Objectives to Bloom’s TaxonomyThe front cover of the revised Bloom’s Taxonomy provides a table in which to map the learningobjectives of a course so as to assist in crafting appropriate teaching and assessment strategies.The numbers in Section III.A and the abbreviations EU, IMP, and FAM to represent EnduringUnderstanding, Important-to-Know, and Good-to-be-Familiar-With concepts
Paper ID #13398Nano-satellites and HARP for Student Learning and ResearchDr. Hank D Voss, Taylor University Dr. Hank D. Voss, Taylor University Dr. Hank D. Voss received his Ph.D. in Electrical Engineering from University of Illinois in 1977. He then worked for Lockheed Palo Alto Research Laboratories prior to coming to Taylor University in 1994. He is currently a Professor of Engineering and Physics at Taylor University. Some of the courses that he regularly has taught include Principles of Engineering, Intro to Electronics, Statics, Advanced Electronics, Jr. Engineering Projects, FE Review, Control Systems
Paper ID #11519Improving Image Quality of a Color Infrared Digital Camera mounted on aSmall UAV Platform: An Iterative Active Learning ExperienceMr. Christopher E Hartman, University of Maryland, Eastern ShoreDr. Abhijit Nagchaudhuri, University of Maryland, Eastern Shore Dr. Abhijit Nagchaudhuri is currently a Professor in the Department of Engineering and Aviation Sciences at University of Maryland Eastern Shore. He is a member American Society for Mechanical Engineers (ASME), American Society for Engineering Education (ASEE) and, American Society for Agricultural and Biological Engineers(ASABE) and is actively involved in
and ejection delay (3). The rocket was observed to be still climbing briefly before beginning its descend, but after the ejection charge. It is reasonable to assume that the remaining time (1.23 seconds) was due to that brief observation. There were 19 other team launches using A8-3 engine. Not all results were as close as the ones reported from this student team report.AVION FLIGHT 25 :Rocket: Avion Engine: B6-4 The model weight: 28.46 g (heavier than most due to optionalspray paint used). Total weight including engine (Wo) = 46.75 grams ,propellant weight (Wp) =6.24 grams Impulse (I) = 5.00 N-s , Thrust Duration (Δt) = 0.8 sec. 1. Average Weight to Burnout (Wb) a. b. Converted to Pounds: 2. Thrust
capacity ofmulti-corner sections under axial compression. Repeated demonstrations of the cardboard Hatcolumn has indicated a range of loading from 14 to 21 books for an impressive collapse load-to-weight ratio of 916 to 1,375.Although the cardboard column demonstration is far from a rigorous scientific experiment, itprovides an impetus to delve deeper into the mathematical analysis and design of thin-walledcolumns as a preamble to more complex stiffened panels as noted below.4. Thin-walled column assignmentAs a basic design-built-test experience, students analyze, build and test two specified thin-walledcolumn (stringer) design concepts with the cross-sectional configurations A & B as shown inFig. 2. This activity is followed by each student
: Classroom-based practicies. Journal of Engineering Education, 94(1):87–101, January 2005.[14] Kenneth A. Bruffee. Collaborative Learning, Higher Education, Interdependence, and the Authority of Knowledge. Johns Hopkins University Press, 1998.[15] Karl Rohnke and Steve Butler. Quicksilver. Project Adventure, Inc. Kendall/Hunt Publishing Co., Dubuque, Iowa, 1st edition, 1995.[16] Brian M. Slator and Harold C. Chaput. Learning by learning roles: A virtual role-playing environment for tutoring. In Intelligent Tutoring Systems, pages 668–676, 1996.[17] B. M. Slator, J. Clark, P. McClean, B. Saini-Eidukat, and A. R. White. Research on role-based learning technologies. In Proceedings. IEEE International Conference on Advanced Learning
Paper ID #14249Putting the Emerging Commercial Sub-orbital Industry to Work for Engi-neering EducationDr. Steven H. Collicott, Purdue University, West Lafayette Professor Collicott has led the proposing, design, and construction of 32 low-gravity NASA aircraft ex- periments, designed 2 of 6 tests in the successful Capillary Fluids Experiments (CFE) performed in the International Space Station in 2006/07, and advised on CFE modifications launched in April 2010. In 2012 he was selected by NASA as PI on the Fluids Education payload for ISS, a new science payload and program in conjunction with a colleague at another school
relatedmodules, while currently subjects are shaped by external logistical factors such as the length of asemester.Outcomes in this model are connected by prerequisite relationships. Any outcome may containpointers to a set of other outcomes which it requires. For an outcome A to require anotheroutcome B, some component of A must require a competency gained in the completion of B.Some outcomes have no prerequisites, and some outcomes have many prerequisites. In this Page 26.1130.5model, prerequisites are considered to be “inherited,” so if outcome A requires outcome B andoutcome B requires outcome C, it is implicit in the model that A requires C and as
). Engineering design: a systematic approach (3rd ed.; K. Wallace & L. Blessing, Eds.). London: Springer. Retrieved from http://link.springer.com/content/pdf/10.1007/3-540- 31629-9_1.pdf doi: 978-1-84628-319-23. Daly, J. R., Augustine, N. R., Davis, J. B., Covert, E. E., & Gray, G. J. (2001). Report to the Panel of to Review the V-22 Program (Tech. Rep.). Arlington, VA: Department of Defense.4. Griffin, J. M. (2005). C-5 Galaxy Systems Engineering Case Study (Tech. Rep. No. September). Wright- Patterson AFB, OH: Air Force Center for System Engineering at the Air Force Institute of Technology.5. Richey, G. K. (2005). F-111 Systems Engineering Case Study (Tech. Rep. No. March). Wright-Patterson AFB, OH: Center for Systems
Paper ID #12399The Role of Radio-Controlled Model Airplanes in the Education of AerospaceEngineersDr. Kathy Schmidt Jackson, Pennsylvania State University, University Park Kathy Jackson is a Senior Research Associate at Pennsylvania State University’s Schreyer Institute for Teaching Excellence. In this position, she promotes Penn State’s commitment to enriching teaching and learning. Dr. Jackson works in all aspects of education including faculty development, instructional design, engineering education, learner support, and evaluation.Dr. Mark D. Maughmer, Pennsylvania State University, University Park Dr. Maughmer
-Steerable Phased Array for Wireless Power Transmission Using a Magnetron Directional Amplifier, 1999 IEEE MTT-S International Microwave Symposium Digest, 1999. 3. Hat- field, M. C., Characterization and Optimization of the Magnetron Directional Amplifier, Doctoral Thesis, University of Alaska Fairbanks, 1999 4. Hatfield, M. C., W. C. Brown, and J. G. Hawkins, Design of an Electronically-Steerable Phased Array for Wireless Power Transmission Using a Magnetron Directional Amplifier, IEEE Proceedings on MTTTS, 1998 5. Hawkins, J. G., S. Houston, M. C. Hatfield, and W. C. Brown, The SABER Microwave-Powered Helicopter Project and Related WPT Research at the Uni- versity of Alaska Fairbanks, Space Technology and Applications