Integrated CubeSat Engineering (2-Days) 4 January - 5 January 2020 Hyatt Regency, Orlando, Florida

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Registration Options:

  • Early Member Rate (until 16 December): $549
  • Standard Member Rate: $649
  • Conference Rate: $749

  • Course Hours:
    0800–1700 hrs

     

    This Integrated CubeSat Engineering course examines the application of Systems Engineering tools and techniques that will provide participants with an understanding of the scope of the skills, industry standards, information, and tools necessary to plan a credible CubeSat Development Program.  Emphasis is on practice over theory using a fully-functional (hardware and software) desktop (non-flight) CubeSat as the system of interest. The course uses the 3U EyasSAT3™ (ES3) desktop satellite (Figure 1), and it follows the progression of a hypothetical CubeSat mission – NanoMet – designed to deliver large scale meteorological imagery from LEO.  NanoMet serves as an end-to-end system engineering and project management training platform to examine issues that develop during each phase of a project lifecycle.  

    Figure 1. EyasSAT3 Layout and Design

    EyasSAT3 Layout and Design 


    The course is organized along the lines of a real space mission, starting with Pre-Phase A concept development and then progressing from Phase A to D, introducing systems engineering artifacts that would be developed at each major milestone and providing hands-on examples using the NanoMet mission. NanoMet, based on the ES3 platform, is designed to conform to the 3U CubeSat standard in terms of form and fit and includes all standard spacecraft bus functions (power, data handling, communication, and 3-axis attitude determination and control). All hardware was designed to be for use around the world and is "ITAR-free," (it is not space-qualified or even qualifiable).  Participants are provided with key lectures and resources and through a variety of in-class exercises will learn by doing.

    Learning Objectives

    • Define mission needs, goals, objectives and ConOps for a CubeSat mission to satisfy Pre-Phase A requirements
    • Develop and organize detailed mission and system requirements as required by a Phase A System Requirements Review (SRR)
    • Describe the tools and techniques needed to develop the complete preliminary design for a CubeSat and conduct a Phase B preliminary design review (PDR)
    • Describe the typical products produced for a critical design review (CDR) at the end of Phase D including system specifications and test plans
    • Implement a typical assembly, integration and test plan for a representative CubeSat system to apply the flow down from requirements to verification activities

    Who Should Attend  

    This course intended for Systems engineers, project managers, integrated product team members involved with any aspect of system engineering and analysis, especially design and development, test and evaluation of CubeSats.

    AIAA CEUs are available for this course.

    Contact

    Please contact Jason Cole if you have any questions about courses and workshops at AIAA forums.

    Outline

    Day 1

    • Intro to Space Systems Engineering 
    • Overview of the NanoMet and the EyasSATSystem of Interest
    • Conceptual Space Mission Design
    • Pre-Phase A Planning
      • Essential Design Review Products
      • Project Scope Definition
    • Engineering Tools and Techniques
    • Requirements Engineering
    • Functional Analysis

    Day 2

    • Orbit Design
    • Spacecraft Subsystems and Sizing
    • Phase B Planning
    • Preparing for Space Systems Verification
    • Phase C/D Planning
    • NanoMet Test Plan
    • NanoMet Simulated Operational Review
    • Course Review and Wrap-up
    Materials

    Course notes will be made available a few days prior to the course event. You will receive an email with detailed instructions on how to access your course notes. Since course notes will not be distributed on site, AIAA and your course instructor highly recommend that you bring your computer with the course notes already downloaded to the course. 

    Each participant will receive:

    • A complete set of course notes with copies of all slides used in the presentations
    • An e-book copy of Applied Space Systems Engineering
    • TSTI Alumni status allowing on-line access to course materials and other resources
    Instructors
    Dr. Peter Van Wirt is a former Deputy Department Head for Labs and Research of the Department of Astronautics at the U.S. Air Force Academy. He has been a visiting lecturer for the Technical University of Delft’s SpaceTech Master’s Degree in Space Systems Engineering and is an Adjunct Professor for the Space Systems Engineering Master’s program at the Stevens Institute of Technology. He also instructs at the National Security Space Institute in Colorado Springs, CO. He has served as a systems engineer/program manager for a variety of US Air Force engineering developments. Peter has over 30 years of aerospace engineering experience and over 20 years teaching experience. He earned his doctorate at the Utah State University.