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It introduces thermodynamics and fluid mechanics, aerodynamics with potential flow and boundary layers, propulsion from engine types to performance analysis, and an aerodynamics laboratory emphasizing measurement and data interpretation. The curriculum progresses to aerospace design and capstone teamwork, then orbital mechanics and spacecraft/spacecraft launch design, followed by aerospace propulsion, aircraft design, stability and control, and structural analysis including finite element and composite methods.",{"@graph":69,"@context":114},[70,84,105],{"@type":71,"itemListElement":72},"BreadcrumbList",[73,77,79,82],{"item":74,"name":75,"@type":76,"position":8},"https://docshare.wps.com","Home","ListItem",{"item":78,"name":9,"@type":76,"position":14},"https://docshare.wps.com/document/",{"item":80,"name":40,"@type":76,"position":81},"https://docshare.wps.com/document/research-report/",3,{"item":83,"name":65,"@type":76,"position":19},"https://docshare.wps.com/document/aerospace-engineering-ae-part-1-course-descriptions/650016/",{"url":83,"name":65,"@type":85,"image":86,"author":91,"headline":65,"publisher":94,"fileFormat":97,"inLanguage":63,"description":67,"dateModified":98,"datePublished":99,"encodingFormat":97,"isAccessibleForFree":100,"interactionStatistic":101},"DigitalDocument",{"url":87,"@type":88,"width":89,"height":90},"https://docshare.wps.com/thumbnails/aerospace-engineering-ae-part-1-course-descriptions/650016.png","ImageObject",300,407,{"name":92,"@type":93},"Mafia Boss","Person",{"url":74,"name":95,"@type":96},"DocShare","Organization","application/pdf","2026-10-30","2026-10-24",true,{"@type":102,"interactionType":103,"userInteractionCount":19},"InteractionCounter",{"@type":104},"ViewAction",{"@type":106,"mainEntity":107},"FAQPage",[108],{"name":109,"@type":110,"acceptedAnswer":111},"What is AE 416 Aerospace Capstone Project and its core requirement?","Question",{"text":112,"@type":113},"AE 416 is a team-based capstone continuing AE 410, where each team designs, fabricates, and tests a multidisciplinary aerospace engineering system to meet customer requirements.","Answer","https://schema.org",{"og:url":83,"og:type":116,"og:title":65,"og:site_name":95,"og:description":67},"article",{"robots":118,"canonical":83},"index,follow",{"doc_id":120,"site_id":62},650016,1792814000,{"code":4,"msg":5,"data":123},{"doc_id":120,"user_id":124,"nickname":92,"user_avatar":125,"doc_module":4,"category_id":39,"category_name":40,"doc_title":65,"doc_description":67,"doc_content":126,"file_id":127,"file_url":128,"file_type":129,"file_size":130,"view_count":19,"is_deleted":4,"is_public":8,"is_downloadable":8,"audit_status":8,"page_count":8,"language":131,"language_code":63,"site_id":62,"html_lang":63,"table_of_contents":132,"faqs":133,"seo_title":134,"seo_description":67,"update_tm":121,"read_time":81},962090760730,"https://ap-avatar.wpscdn.com/davatar_9964176cb1d06d4a9deccf72a44ae3dc","Aerospace Engineering (AE) (AE) 1  \nAEROSPACE ENGINEERING (AE) (AE)   \nAE 260 Aerospace Fundamentals 3 cr  \nIntroduction to the fundamental concepts of thermodynamics and fluid mechanics for applications to aircraft and spacecraft design and performance analysis.  \nPrerequisite: PH 201 Minimum Grade of C and MA 227 Minimum Grade of C  \nAE 361 Fundamentals of Aerodynamics 3 cr  \nConservation laws, potential flow, airfoil and wing analysis. Boundary layer theory and pressure gradients on plates and airfoils. Introduction to turbulent and vortex-dominated flows.  \nPrerequisite: (EG 360 Minimum Grade of C and MA 227 Minimum Grade of C and PH 202 Minimum Grade of C)  \nAE 366 Aerospace Propulsion 3 cr  \nThis course covers basic one-dimensional flows related to aircraft and rocket engines. The types of engines include propeller driven engines, ramjets, turbojets, turbofans, turboprops and rockets as well as advanced propulsion such as solar sails and ion thrusters. Performance analysis is done on all of these engines as well as performance characteristics of inlets, exhaust nozzles, compressors, burners, and turbines in jet engines. This course also includes an Introduction to hobbyist rocket design using the design, build, test framework.  \nPrerequisite: AE 260 Minimum Grade of C and AE 361 (may be taken concurrently) Minimum Grade of C  \nAE 371 Aerodynamics Laboratory 1 cr  \nExperimental laboratory in solid and fluid mechanics, aerodynamics, propulsion. Emphasis on measurement techniques, analysis and interpretation of data, comparison to analytical predictions, and reporting. Prerequisite: AE 361 Minimum Grade of D and EH 102 Minimum Grade of C  \nAE 410 Principles of Aerospace Design 3 cr  \nIntroduction to aerospace design, including an understanding of the various subsystems for all types of aerospace systems and how the overall vehicle's optimization leads to good conceptual designs. Introduction to parameters in aerospace analysis and how they affect the design. Introduction to the systems engineering design process. Prerequisite: EH 102 Minimum Grade of C and EG 231 Minimum Grade of D and ME 326 Minimum Grade of D and AE 366 Minimum Grade of Cand AE 371 Minimum Grade of D and AE 425 (may be taken concurrently) Minimum Grade of D and AE 469 (may be taken concurrently) Minimum Grade of D  \nAE 416 Aerospace Capstone Project 3 cr  \nThis is a team-based capstone project course and a continuation of AE 410. Each team is assigned a multidisciplinary aerospace engineering project, involving the design, fabrication, and testing of a system to meet customer requirements.  \nPrerequisite: AE 410 Minimum Grade of DAE 425 Orbital Mechanics 3 cr  \nThe course is an introduction to orbital and trajectory design. Topics include: Newton’s law of gravity; relative equations of motion; conic sections; orbits in three dimensions; impulsive maneuvers; transfer orbits; patched conics; Lambert’s theorem.  \nPrerequisite: MA 238 Minimum Grade of C and EG 284 Minimum Grade of  \nAE 464 Principles of Spacecraft Desgn 3 cr  \nIntroduction to space launch vehicle and spacecraft design, including an understanding of the various subsystems and how the overall vehicle's optimization leads to good conceptual designs. Introduction to parameters in aerospace analysis and how they effect the design. Prerequisite: (ME 228 Minimum Grade of C and EG 360 Minimum Grade of C)  \nAE 466 Principles of Aerospace Propulsion 3 cr  \nAirbreathing engines course. Apply fluids, thermodynamics, and heat transfer to analysis of air breathing engines. Topics to include: ideal cycle analysis, component performance, non-ideal cycle analysis, and blade aerodynamics.  \nPrerequisite: ME 312 Minimum Grade of D and EG 360 Minimum Grade of D and ME 317 (may be taken concurrently) Minimum Grade of D  \nAE 468 Principles of Aircraft Design 3 cr  \nIntroduction to aircraft design, including an understanding of the various components leading to a good conceptual design. Introduction to parameters i","cbCaisNvjtwwlEYQ","https://ap.wps.com/l/cbCaisNvjtwwlEYQ","pdf",57281,"English","# Course Catalog Overview\n## AE 260 - Aerospace Fundamentals\n## AE 361 - Fundamentals of Aerodynamics\n## AE 366 - Aerospace Propulsion\n## AE 371 - Aerodynamics Laboratory\n## AE 410 - Principles of Aerospace Design\n## AE 416 - Aerospace Capstone Project\n## AE 425 - Orbital Mechanics\n## AE 464 - Principles of Spacecraft Design\n## AE 466 - Principles of Aerospace Propulsion\n## AE 468 - Principles of Aircraft Design\n## AE 469 - Aircraft Stability and Control\n## AE 470 - Aircraft Structural Analysis","[{\"question\":\"What is AE 416 Aerospace Capstone Project and its core requirement?\",\"answer\":\"AE 416 is a team-based capstone continuing AE 410, where each team designs, fabricates, and tests a multidisciplinary aerospace engineering system to meet customer requirements.\"}]","Aerospace Engineering (AE) - Part 1 - Course Descriptions | PDF"]