CubeSat and ThinSat – Introduction, Applications, and Methods for Mission Success
Interactive Course with Hands-On Design and Analysis
February 24-25, 2020 | Denver, CO

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Overview

Includes a Customized Design, Build, and Flight Test With Live Data Feedback

This 2-day academic course with a hands-on workshop provides an overview of the rapidly growing and disruptive small satellite space industry including overviews on multi-CubeSat and smaller ThinSat form factors. This short course will provide an outline of the systems engineering approach to develop a space mission using small satellites from Low Earth Orbit (LEO) (including reentry) to Geostationary Orbit (GEO), as well as interplanetary missions. Along with these objectives, attendees will also be given an overview of the space environment (plasma, charging, thermal, radiation, dose, etc…) and how it’s effects performance. This is a new, one-stop shop for space stakeholders to learn how to mitigate design problems, design a satellite based on mission and specific requirements, and achieve flight lineage through mission success the first time.

Learning Outcomes and Objectives:

  • Review Technology trends in the Space Program and CubeSat and ThinSat concepts
  • Landscape Assessment of the Space environment and environmental damage mitigation from LEO to GEO for satellite hardware
  • Explore basics of Small spacecraft power systems design: Solar Cells, peak trackers, batteries, power management, Inhibits, and related firmware
  • Assess the Simplex unit, it’s applications and advantages, and a comprehensive cost/benefit analysis of various satellite communication systems and room for improvement
  • Review CubeSat mechanical and structure design fundamentals including manufacturing requirements, materials ODAR, simulations, and safety reviews
  • Formulate a viable and customized satellite concept, build, and mission schedule
  • Discuss how new Advanced Manufacturing (AM), miniaturization, and high-quality robotic mass production with many new and competitive launch opportunities make
  • Cube/Thin Sats an affordable technology
  • Discuss novel and successful Systems Engineering design practices for a small space mission
  • Assess subsystem and sensor options: GPS, Black Box, Attitude Determination and Control, and Propulsion
  • Discuss small spacecraft environmental testing, launch requirement documents and Launch Readiness Review
  • Review orbits, launch, Con-Ops, ground segments, and data analysis
  • Day 2: Build your own ThinSat, connect with a satellite network, and record your ThinSat data on a laptop in near real-time

Day 2 Technical Design, Build, Flight Test and Live Data Feedback

  • Review Personalized Satellite Builds and Provide Feedback
  • ThinSat Kit includes 3D printed structure, Solar Array Circuit Boards, Processor,
    Wi-Fi link, Ground Station software, Electrical power system, few Solar arrays
    with Peak Power trackers, Battery, magnetic attitude, and other subsystems.
    In addition, sensors include light, UV, IR sensors, energetic particle sensor,
    temperature, Inertial Motion Sensor (3-axis gyros, 3 accelerometers, and 3 magnetometers)
  • Complete building of your individual EM ThinSat
  • Testing and calibration of your ThinSat. Record live data on your ground station laptop
  • One-on-one supervision and help from instructors

Requirements For Successful Completion Of Program

Participants must sign in/out each day and be in attendance for the entirety of the conference to be eligible for continuing education credit. Regular interaction with course instructor indicating comprehension of the subject matter being taught.

Instructional Methods

Case studies, PowerPoint presentations, and learning exercises will be used in this program.

ROI for Attendees:

The material provided for the course will include a manual of all the slides presented, a reference list of small satellite companies, small satellite parts vendors and institutions that are recommended for additional graduate training. In addition, the lab portion of the class will include a full 3D printed ThinSat that will have a processor and sensor PC board that will be launched on a high-altitude balloon tether for collecting data for ground station display.

There will be a hands-on display of some of the current component technology that can be purchased from national and international vendors (Structures, Solar arrays, trackers, foldouts, Electrical Power Systems, Batteries, Communication systems, antennas, Globalstar, Attitude control systems, mechanisms, GPS, propulsion, and flight processors and software).

Audience:

This course is intended for new engineers and managers that have a technical background but are not intimately familiar with the requirements of space mission design and design of small spacecraft. Further titles should include: Engineers, managers, and investors involved in spaceflight satellite systems or thinking about building a full CubeSat or a satellite subsystem, professionals interested in satellite technology or manufacturing, other technical staff, educators, and stakeholders.

Agenda

Monday, February 24, 2020

8:00 – 8:30 am :: Registration and Continental Breakfast

8:30 am – 5:00 pm :: Course Timing

12:00 – 1:00 pm :: Group Luncheon


Introduction

  • General introduction to small satellite space industry
  • Discuss key variables to a satellite project lifecycle including costs, timeline, and componentry
  • Review CubeSat and ThinSat form factors
  • Space environment
  • Overview of space environment and mitigation from LEO to GEO for satellites
  • Review technology trends in the space program and CubeSat and ThinSat concepts
  • Space debris considerations

System Engineering Tradeoffs

  • Understand novel and successful systems engineering design practices for a small space mission
  • PDR and CDR reviews
  • Interface Control Documents (ICD)

Electrical Power Systems (EPS)

  • Learn basics of small spacecraft power systems design
    • Solar cells – PV
    • Peak trackers
    • Batteries
    •  Power management
    •  Inhibits
    • Other related firmware

Communication and Antenna System Design with Licensing

  • Various methods for satellite telemetry and comm coverage
  • Tradeoffs with various communications systems:
    •         Antennas, TX and RX link margins, EPS
    •         FCC and ITU requirements
    •         Data rates, resource requirements, and approx. costs
    •         Coverage costs, latency, with different sat constellations
  • Simplex Unit
    • Introduction to design, applications, and key contributions of a simplex communication unit
    •  Transmission to ground station
    •   Simplex vs. duplex attributes and analysis

Mechanical and Materials Requirements

  • CubeSat mechanical and structure design
    • CAD software demonstration
    • Visual representation of successful mission features
  • Manufacturing requirements
    • Compliance and vendor componentry expectations
    • Communication strategies for efficient collaboration between manufacturer and assembly team
  • Materials for formulating Orbital Debris Assessment Report (ODAR)
  • Simulations
  • Safety reviews

Subsystems and Payloads

  • Subsystem and sensor options:
    • GPS
    • Black Box
    • Communication (simplex, duplex…)
    • Altitude determination and control
    •  Propulsion systems
      •  Iodine hall thrusters
      • Pulsed plasma thrusters
      • Cold gas

Design a Customized Satellite Plan

  • Design a personalized satellite concept and build timeline
  • Put together milestone schedule for on-time mission plan
  • Develop design pitfalls and identify necessary adjustments alongside instructors

Environmental Testing Requirements

  • Small spacecraft environmental testing
  • Launch requirement documents and Launch Readiness Review (MRR)
  • Safety and license requirements review
  • Structural testing methods
    • Radiation
    •  Vacuum
    • Vibration

Orbits and Con-Ops

  • Orbital satellite activation
    • Monitor points
  • Orbits programs, two line elements
  • Launch and con-ops
  • Ground station segment data and data analysis

 Tuesday, February 25, 2020

8:00 – 8:30 am :: Continental Breakfast

8:30 am – 5:00 pm :: Technical Design, Build, Flight Test and Live Data Feedback

12:00 – 1:00 pm :: Group Luncheon


ThinSat Introduction & Overview

    • 3D printed structure
    • Solar array circuit board
    • Processor
    • Wi-Fi link
    • Ground station software
    • Electrical power system
    • Few solar arrays with peak power trackers
    • Battery
    • Magnetic attitude
    • Other subsystems

Assemble ThinSat Bus system in 3-D Printed frames

    • Work alongside instructors to develop customized, printed hardware for ThinSat
    • Review personalized satellite builds and provide feedback

Calibrate Sensors

    • Connect bus and sensors with ground station laptop
    • Transmit and test data over the Globalstar network to ground station
    • Sensors include:
      • Light
      • UV
      • IR sensors
      • Energetic particle sensor
      • Temperature
      • Inertial motion sensor (3-axis gyros, 3 accelerometers, and 3 magnetometers)

Complete Assemblage of Individual EM ThinSat


Testing and Calibration of ThinSat

    • Record live data on ground station laptop
    • Receive feedback on data analysis and findings

Closing Remarks and Final Q&A

 

Instructors

Dr. Hank Voss
CEO and Chief Scientist, NearSpace Launch Inc. (NSL)

Dr. Hank Voss is an Emeritus Professor in Engineering and currently CEO and Chief Scientist at NearSpace Launch Inc. (NSL) located in Upland, IN. In the past 5 years NSL has created and launched 350 CubeSat subsystems and developed over 10 full satellites with 100 % success in-orbit. NSL was also the first to demonstrate the powerful Globalstar satellite-to-satellite link for 24/7 anywhere-anytime global visibility of a satellite with low latency of a few seconds. He worked previously 15 years at Lockheed Research Labs in Palo Alto CA on many advanced NASA and DOD satellites and payloads. Dr. Voss worked with Prof. Twigg, Inventor of the CubeSats, in the early days of CubeSats at Stanford and was instrumental in developing the first 2U CubeSat with students. He has 22 years’ experience in teaching aerospace and engineering at Taylor University in IN and development of many small spacecraft in an academic environment while receiving the university Teaching Excellence award and Forman Research award. While in Indiana he launched Indiana’s first satellite and first commercial satellite. He is an inventor of the new ThinSat standard to significantly reduce cost for access to space and inventor of the new thin patch satellite Black Box for mission success, diagnostics, and space debris GPS tracking. He has been responsible for the development of eleven small satellites (1U to 6U) that were launched into LEO orbit with a 24/7 Globalstar communication link that needs no ground station since all the encrypted data is linked through the internet. NSL has developed 60 autonomous ThinSats that launched as a constellation in 2019 with Professor Twiggs as well as a CubeSat payload for Deep Space and lunar flyby on the EM-1 mission.

He has a BS in Electrical Engineering from the Illinois Institute of Technology and a MS and PhD in Electrical Engineering from University of Illinois. He has published over 150 technical papers in Space Science, Space Instrumentation and CubeSat results.

Secondary instructors include:

Matt Orvis BS, MS
Project Engineer, NearSpace Launch Inc. (NSL)

Mr. Matt Orvis BS and MS in Physics/Engineering and a project engineer with NearSpace Launch. Matt has worked over 5 years with state-of-the-art satellite design and acted as the lead engineer for the THEEF subsystem, an electric field and VLF sensor. He has been involved in the design and build of numerous other small satellites ranging from ThinSats to 6Us and 12Us.

Course Support:

Bob Twiggs
President and Founder, Twiggs Space Labs

Bob Twiggs, president and founder at Twiggs Space Labs and widely regarded as the founder and instigator to the original CubeSat concept. Twiggs is presently a professor of astronautical engineering in the Space Science Center at Morehead State University in Morehead, Kentucky. Prof. Twiggs was a consulting professor at Stanford University Department of Aeronautics and Astronautics starting in 1994 where he established the Space Systems Development Laboratory.


Matt Craft
President, Craft Consulting, LLC

Matt Craft has over twenty-five years of business experience with a specialization in new business startups, financing, business strategy and planning, including over nine years of experience in the legal and financial industries and sixteen years supporting and guiding numerous entrepreneurial ventures through the various stages of growth and acquisition.

Location

Plaza Tower One Conference Center

6400 S Fiddlers Green Cir.

Greenwood Village CO, 80111

The conference center is conveniently located adjacent to the Arapahoe at Village Center Light Rail Station, allowing easy access to and from DIA, Downtown, and Local Area Attractions.

Nearby Hotels

Each of these hotels offers a complimentary shuttle to and from the conference center.

Springhill Suites DTC
7900 East Peakview Ave
Greenwood Village, CO 80111
Phone: 303-721-3321
0.3 miles away

Wingate by Wyndham
8000 East Peakview Ave
Greenwood Village, CO 80111
Phone: 303-626-2641
0.3 miles away

Hyatt Place Denver Tech Center
8300 E.Crescent Parkway
Greenwood Village, CO 80111
Phone: 1-303-804-7000
2.1 miles away

Hyatt Regency Denver Tech Center
7800 East Tufts Ave
Denver, CO 80237
Phone: 1-303-779-1234
2.8 miles away

Denver Marriott Tech Center
4900 S Syracuse St
Denver, CO 80237
Phone: 303-779-1100
3.1 miles away

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