This course studies the basic principles of propulsion systems with emphasis on jets and fan systems. It also includes the study of inlets and nozzles, compressors, burners, fuels, turbines and jets culminating in design and off-design engine analysis, performance and environmental considerations. The impact of propulsion system integration on external aerodynamics and (noise and IR) signature reduction is also presented, along with an introduction to novel concepts in propulsion.September 8-12, 2025, San Diego Marriott Mission Valley
This course provides an overview of aircraft structural external loads analysis including: criteria, design, analysis, fatigue, certification, validation, and testing. It covers CFR Part 25 airplane load requirements and the historical CFR Part 23 requirements which are the basis of the current ASTM standards. These concepts are applicable to many military structural requirements, UAV's, and other experimental or novel configuration aircraft.
This course provides an introduction to the analysis and design of aircraft structures. Course content includes design criteria, structural design concepts, loads and load paths, metallic and composite materials, static strength, buckling and crippling, durability and damage tolerance, practical design considerations, certification and repair. Analysis exercises and a design project are included to better involve students in the learning process.
This course provides a conceptual approach to the overall design of Unmanned Aircraft Systems (UAS) including concepts of operations, communications, payloads, control stations, air vehicles and support. It also covers requirements and architecture development, initial sizing and conceptual-level parametric and spreadsheet assessment of major system elements.September 8-10, 2025, San Diego Marriott Mission Valley
This course discusses the FAA Code of Federal Regulations (CFRs) and design concepts required to ensure all aspects of aircraft electrical wiring and installation are safe. It examines aircraft wiring as a system and reviews all Part 25 CFRs related to EWIS FAA certification.
This course covers fundamental design issues, along with analysis and design methodologies for aerospace hydraulic and flight control systems. Topics include design requirements, component description and operation, component and system math modeling, component sizing, system layout rationale, system sizing and airframe integration. The course emphasizes the fundamentals and necessary engineering tools (both analytical and otherwise) needed to understand and design aerospace hydraulic and flight control systems.
This course will provide an overall understanding of the 14 CFR Part 21 requirements necessary to obtain design, production and airworthiness approvals for civil aviation products and articles. Title 14, CFR Part 21 regulations are the backbone of the regulatory framework that enables Aircraft Certification Service (AIR) to conduct its certification responsibilities on products and articles. Under 14 CFR Part 21, §21.1, the FAA defines a product as an aircraft, engine or propeller, while an article means a material, part, component, process or appliance. In addition to 14 CFR Part 21, this course will delve into certain aspects of 14 CFR Part 43, outlining the requirements to receive approval for alterations/repairs for civil aviation products and articles. An overview is provided on FAA organizational structure, additional 14 CFR Parts, regulatory/guidance material, and rulemaking procedures. March 17-20, 2025, DoubleTree Suites by Hilton Hotel Seattle Airport Southcenter September 8-11, 2025, San Diego Marriott Mission Valley
This course provides details on all elements of fuel tank design needed for compliance with the related regulations, with specific emphasis on electrical design aspects. Some review of regulatory history of 25.954 and 25.981 up to Amendment 25.146 is included for reference for TC, ATC, and STC activities, while the main emphasis of this course will explore the guidance material for fuel tank safety compliance provided within the FAA advisory circulars and SAE ARP6205 document.September 8-12, 2025, San Diego Marriott Mission Valley
This course is designed to provide a qualitative understanding of aeroelastic behavior for aerospace vehicles. The class will explore different forms of aeroelastic phenomena and associated issues in structural dynamics and aerodynamic-structure interaction. The level of class instruction is appropriate for engineers and managers with an undergraduate degree in engineering.September 8-12, 2025, San Diego Marriott Mission Valley