Vibration Testing of Small Satellites
Short Course Immediately Following the SmallSat Conference

August 10, 2017, 2:00 - 6:00 PM
August 11, 2017, 8:30 AM - 5:00 PM
Eccles Conference Center, Logan, UT
Refreshments and Friday Lunch Provided

Course Overview:
This new 12-hour course provides a tutorial, practical guidance, examples, and recommendations for testing a small satellite on an electrodynamic shaker. Addressed are sine-burst testing, random vibration testing, and low-level diagnostic sine sweeps. Notching, response limiting, and force limiting are addressed in detail, with examples. The course is primarily aimed at satellites in the 50 - 500 lb (23 - 230 kg) range, but it also applies to CubeSats. Most of the guidance applies to larger satellites as well if they will be tested on a shaker.

Course Objectives:
  • establish an effective vibration test program
  • identify and clearly state test objectives
  • design (or recognize) a test that satisfies the objectives while minimizing risk of an over test
  • establish pass/fail criteria and interpret test data
  • write effective test plans and test reports
  • build stakeholder confidence and get buy-in

Course Length:
One and one-half days

Target Audience:
All engineers & managers involved in ensuring small spacecraft can withstand launch environments