CC Sumer 2018 Challenge. Unmentionables: Dr. Gary Snyder, an actual rocket scientist.
Lyrics
Launch systems ready
Check reaction control system
Simulation is no substitute
Countdown to ignition
All Systems Go
Random and chaotic attitude heading during cubesat deployment with a predominant bias toward lateral relative velocity vectors leads to a half or full orbit recontact event for each payload.
Monte carlo simulations are no substitute for analytical analysis of the deployment scenario. If we don't fly, nobody flies
Thrust vector control
Ballistic coefficient
Divergent pressure anomaly;
Shake and bake was insufficient